| AUTHOR NAME |
PAPER TITLE |
ICAS PAPER NUMBER |
| Aakkula,
J. |
DIARC PLASMA COATING FOR
RELIABLE AND DURABLE STRUCTURAL BONDING OF METALS |
ICAS2012-7.2.1 |
| Abdalla, A. M. |
THE INFLUENCE OF DEMOISELLE
AIRCRAFT ON LIGHT AND GENERAL AVIATION DESIGN |
ICAS2012-1.7.ST |
| Abdalla, A. M. |
AIRCRAFT EMERGENCY
EVACUATION SIMULATION USING ANT COLONY OPTIMIZATION |
ICAS2012-9.1.3 |
| Abdi, F. |
COUPLED
MICROMECHANICS-FINITE ELEMENT PROGRESSIVE FAILURE DYNAMIC ANALYSIS APPROACH:
F-16 CANOPY CASE STUDY |
ICAS2012-7.7.5 |
| Abdi, F. |
REAL
TIME DIAGNOSIS OF DYNAMIC FAILURE IN FUTURE AEROSPACE STRUCTURES |
ICAS2012-8.11.2 |
| Abe, H. |
MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1.ST2 |
| Abedian, A. |
EFFECT OF LATERAL PLACEMENT
OF CERAMIC AND METAL GRAINS ON THERMAL STRESS DISTRIBUTION THROUGHOUT FGMS |
ICAS2012-7.3.4 |
| Abedian, A. |
FINDING TUNING FREQUENCY OF
SYMMETRIC AND ANTI-SYMMETRIC LAMB WAVES USING FEM |
ICAS2012-P3.6 |
| Abedian, A. |
WAVELET-BASED ACTIVE SENSING
FOR QUANTITATIVE ASSESSMENT OF THROUGH-THICKNESS CRACK SIZE AND ANGLE IN
COMPOSITE PLATES |
ICAS2012-P3.8 |
| Abedian, A. |
RISK ASSESSMENT MODELLING
FOR EVALUATING SAFETY AND IMPACT ON BUSINESS VIA A 3D RISK MATRIX |
ICAS2012-P9.2 |
| Abramov, N. |
AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS2012-3.1.2 |
| Abramov, N. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
| Abu Talib, A. R. |
PERFORMANCE TEST OF A
SMALL-SCALE TURBOJET ENGINE RUNNING ON A PALM OIL BIODIESEL - JET A BLEND |
ICAS2012-4.8.1 |
| Achard, P. |
APACHE : INTEGRATED HYBRID
FUEL CELL SYSTEM FOR 2-SEAT ALL ELECTRIC AIRCRAFTS PROPULSION |
ICAS2012-6.7.4 |
| Adachi, K. |
INTEGRATED DESIGN METHOD OF
A ROCKET ENGINE TURBOPUMP SUB-SYSTEM FOR SUPPRESSING ROTOR LATERAL VIBRATION |
ICAS2012-4.3.4 |
| Adamczak, D. |
HIFIRE-1 BOUNDARY-LAYER
TRANSITION MEASUREMENTS |
ICAS2012-3.10.3 |
| Adams, N. |
AERODYNAMIC OPTIMISATION OF
A MORPHING MEMBRANE WING |
ICAS2012-3.6.3 |
| Adams, N. A. |
FLOW CHARACTERISTICS OF A
HELICOPTER FUSELAGE CONFIGURATION INCLUDING A ROTATING ROTOR HEAD |
ICAS2012-2.7.3 |
| Adams, N. A. |
AEROACOUSTIC ANALYSIS OF A
HELICOPTER CONFIGURATION WITH DUCTED TAIL ROTOR |
ICAS2012-3.9.1 |
| Agarwal, R. K. |
ACTIVE
CONTROL OF SHOCK/BOUNDARY LAYER INTERACTION FOR TRANSONIC DRAG REDUCTION OF
AIRFOILS |
ICAS2012-2.10.4 |
| Agusdinata, D. B. |
DEVELOPING OPTIMAL AIRLINE
FLEETS UNDER ENVIRONMENTAL AND CAPACITY CONSTRAINTS |
ICAS2012-7.10.1 |
| Ahmad, M. T. |
PERFORMANCE TEST OF A
SMALL-SCALE TURBOJET ENGINE RUNNING ON A PALM OIL BIODIESEL - JET A BLEND |
ICAS2012-4.8.1 |
| Ai, J. |
RESEARCH ON ESTIMATING
METHOD OF FUEL AND EMISSIONS USING NEURAL NETWORKS IN LTO CYCLE FOR
PRELIMINARY AIRCRAFT DESIGN |
ICAS2012-7.11.2 |
| Aksaray, D. |
STATISTICAL STABILITY AND
CONTROL ANALYSIS TO INVESTIGATE THE CONTROL EFFORT OF IMPROVING HANDLING
QUALITY CHARACTERISTICS |
ICAS2012-5.9.1 |
| Alderliesten, R. C. |
ENERGY DISTRIBUTION IN GLARE
AND 2024-T3 ALUMINIUM DURING LOW-VELOCITY IMPACT |
ICAS2012-7.7.2 |
| Alers, T. |
AN ASSET FOR IMPROVED
EFFICIENCY AND PUNCTUALITY IN AIR TRANSPORT |
ICAS2012-11.7.5 |
| Allain, L. |
RELIABILITY ANALYSIS OF
AIRCRAFT SYSTEM ARCHITECTURES |
ICAS2012-P9.1 |
| Allwood, G. |
DISTRIBUTED
OPTICAL FIBRE SMART SENSORS FOR ADVANCE SENSING SYSTEMS IN AEROSPACE VEHICLES |
ICAS2012-P6.7 |
| Alonso, J. J. |
COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS2012-1.9.1 |
| Altunlu, A. C. |
ACCELERATED LIFE CONSUMPTION
DUE TO THERMO-ACOUSTIC OSCILLATIONS IN GAS TURBINES: XFEM & CRACK |
ICAS2012-4.2.2 |
| Alvarez, L. M. |
EXTRACTING DECK TREND TO
PLAN DESCENT TRAJECTORY FOR SAFE LANDING OF UAVS |
ICAS2012-11.8.3 |
| Alwi, S. I. S. |
PRODUCTION
OF BIO-FUEL FROM ALGAE BIOMASS, NANNOCHLOROPSIS OCULATA, FOR ADDITION TO
KEROSENE JET A-1 |
ICAS2012-8.6.4 |
| Amadori, K. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
| Aminanda, Y. |
MODELLING OF IMPACT ON
SANDWICH STRUCTURE FOR FAST MAINTENANCE LOOPS |
ICAS2012-8.3.3 |
| Amiryants, G. |
AEROELASTIC
MULTIDISCIPLINARY ANALYSIS OF THE FIN
WITH INNOVATIVE ADAPTIVE CONTROL |
ICAS2012-8.7.4 |
| Anderson, D. |
ASSESSING
HELICOPTER SURVIVABILITY TO GROUND LAUNCHED PROJECTILES USING MULTI-FIDELITY
INVERSE SIMULATION |
ICAS2012-1.4.4 |
| Anderson, D. |
DEVELOPMENT OF NAVIGATION
ALGORITHMS FOR NAP-OF-THE-EARTH UAV FLIGHT IN A CONSTRAINED URBAN ENVIRONMENT |
ICAS2012-11.9.1 |
| Andreeva-Mori, A. |
A STUDY ON FINDING A
SUBSTITUTE TO THE FIRST COME- FIRST SERVED RULE APPLIED TO AIRCRAFT
SEQUENCING |
ICAS2012-10.8.2 |
| Anemaat, W. A. J. |
DESIGN METHODS FOR AN
UNCONVENTIONAL SPLIT WING AIRCRAFT CONFIGURATION |
ICAS2012-1.3.1 |
| Anghileri, M. |
EXPERIMENTAL AND NUMERICAL
ASSESSMENT OF HELICOPTER SUBFLOOR CRASHWORTHINESS |
ICAS2012-8.1.1 |
| Anghileri, M. |
PRELIMINARY INVESTIGATION ON
THE FEASIBILITY OF A BIRD SURROGATE FOR FULL-SCALE BIRD IMPACT TEST |
ICAS2012-8.3.1 |
| Anton, E. |
AN INTERDISCIPLINARY
APPROACH FOR A VIRTUAL AIR-TRAFFIC SYSTEM SIMULATION FOR SUBJECTIVE
ASSESSMENT IN VR ENVIRONMENTS |
ICAS2012-7.10.3 |
| Antunes, A. P. |
ON THE EFFECTS OF TURBULENCE
MODELING AND GRID REFINEMENT ON HIGH-LIFT CONFIGURATION AERODYNAMIC
SIMULATIONS |
ICAS2012-2.3.1 |
| Aoki, Y. |
EVALUATION ON DISCRETE
SOURCE DAMAGES OF CFRP STIFFENED PANELS |
ICAS2012-7.7.1 |
| Aoyama, S. |
DEVELOPMENT OF MOBILE
PASSIVE SECONDARY SURVEILLANCE RADAR |
ICAS2012-P8.8 |
| Aoyama, T. |
DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11.ST |
| Appel, B. |
UAS DESIGN REQUIREMENTS FOR
OPERATION IN COLOMBIAN MOUNTAIN ENVIRONMENTS |
ICAS2012-1.8.ST |
| Arai, N. |
COMPARISON OF PERFORMANCE OF
PROPELLER BLADES BY DIFFERENCE IN PLANAR SHAPE |
ICAS2012-4.6.ST1 |
| Archambaud, J. -P. |
STABILITY ANALYSIS ON
NATURAL LAMINAR FLOW WING IN SUPERSONIC FLOW: ONERA-JAXA JOINT RESEARCH
PROGRAM |
ICAS2012-3.10.1 |
| Arevalo, J. L. L. |
WEIGHT ON WHEEL SYSTEM BASED
ON STRAIN GAUGES |
ICAS2012-6.11.2 |
| Arimoto, M. |
EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS2012-9.3.1 |
| Arnal, D. |
STABILITY ANALYSIS ON
NATURAL LAMINAR FLOW WING IN SUPERSONIC FLOW: ONERA-JAXA JOINT RESEARCH
PROGRAM |
ICAS2012-3.10.1 |
| Arnaldo, R. |
HALA!: TOWARDS HIGHER LEVELS
OF AUTOMATION IN ATM. POSITION PAPER -STATE OF THE ART AND RESEARCH AGENDA |
ICAS2012-10.1.1 |
| Arnaldo, R. |
AIRCRAFT FLIGHT TRAJECTORY
DEVIATION IN THE STANDARD INSTRUMENT DEPARTURES. OPERATORS PENALTIES |
ICAS2012-10.10.2 |
| Arnaldo, R. |
LEGAL AND TECHNICAL
IMPLICATIONS OF THE SAFETY RECOMMENDATIONS ISSUED IN THE FINAL REPORTS OF THE
CIVIL AIR ACCIDENTS AND INCIDENTS INVESTIGATIONS |
ICAS2012-9.4.ST |
| Asai, K. |
MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1.ST2 |
| Aso, S. |
EXPERIMENTAL STUDY OF THE
MORPHING FLAP AS A LOW NOISE HIGH LIFT DEVICE FOR AIRCRAFT WING |
ICAS2012-9.11.3 |
| Atencio, B. N. |
MEASUREMENTS AND PREDICTION
OF LAMINAR-TURBULENT TRANSITION AT HIGH FREE-STREAM TURBULENCE & PRESSURE
GRADIENTS |
ICAS2012-3.10.5 |
| Atinault, O. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
| Atkin, C. J. |
RECENT DEVELOPMENTS TO THE
VISCOUS GARABEDIAN AND KORN METHOD |
ICAS2012-2.11.3 |
| Atobe, T. |
STABILIZING EFFECT OF
LONGITUDINAL-WALL OSCILLATION ON 2D CHANNEL FLOW |
ICAS2012-P2.12 |
| Attia, M. |
PRE-STRESSED MODAL ANALYSIS
OF A TURBINE SPACER |
ICAS2012-P4.11 |
| Aubert, S. |
TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS2012-4.4.4 |
| Aubert, S. |
DERIVATED TURBULENCE MODEL
TO PREDICT HARMONIC LOADS IN TRANSONIC SEPARATED FLOWS OVER A BUMP |
ICAS2012-4.6.4 |
| Aubry, S. |
MODELLING AIR TRAFFIC IMPACT
ON LOCAL AIR QUALITY WITH IESTA AND ADMS-AIRPORT: VALIDATION USING FIELD
MEASUREMENTS ON A REGIONAL AIRPORT |
ICAS2012-4.9.4 |
| Avakyan, A. |
A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS2012-6.11.3 |
| Azevedo, J. L. F. |
ON THE EFFECTS OF TURBULENCE
MODELING AND GRID REFINEMENT ON HIGH-LIFT CONFIGURATION AERODYNAMIC
SIMULATIONS |
ICAS2012-2.3.1 |
| Bae, J. C. |
THERMAL ANALYSIS NEAR
SECONDARY INJECTION HOLE IN SITVC SYSTEM |
ICAS2012-P4.9 |
| Baena, S. |
COLD FUEL TEST RIG TO
INVESTIGATE ICE ACCRETION ON DIFFERENT PUMP INLET FILTER-MESH SCREENS |
ICAS2012-6.5.2 |
| Bagassi, S. |
DESIGN ANALYSIS FOR HYBRID
PROPULSION |
ICAS2012-6.7.5 |
| Bagassi, S. |
INNOVATION IN MAN MACHINE
INTERFACES: USE OF 3D CONFORMAL SYMBOLS IN THE DESIGN OF FUTURE HUDS (HEAD UP
DISPLAYS) |
ICAS2012-9.7.2 |
| Bagassi, S. |
A
META-HEURISTIC APPROACH TO SIMULATE TAXI OPERATIONS |
ICAS2012-P8.7 |
| Bagg, R. L. |
DEVELOPMENT OF A
HYBRID-ELECTRIC POWER-SYSTEM MODEL FOR A SMALL SURVEILLANCE AIRCRAFT |
ICAS2012-P6.4 |
| Bai, J. |
APPLICATION
OF TWO TRANSITION MODELS TO FLOWS AROUND AIRFOILS |
ICAS2012-2.4.4 |
| Bain, M. |
ENGINE-OUT TAKEOFF PATH
OPTIMIZATION OUT OF TERRAIN CHALLENGING AIRPORTS |
ICAS2012-5.8.2 |
| Bakar, A. |
MULTIDISCIPLINARY EVALUATION
OF TRUSS-BRACED WING FOR FUTURE GREEN AIRCRAFT |
ICAS2012-1.10.ST |
| Baker, J. |
SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS2012-7.2.2 |
| Baker, J. W. C. |
DEVELOPING THE USE OF
NEURAL-NETWORK TEST TECHNOLOGY FROM AVIONICS TO WIRING SYSTEMS |
ICAS2012-12.5.1 |
| Bakker, G. J. |
ANALYZING SEPARATION LOSS
EVENTS IN TWO-PAIRED AIRCRAFT TRAILING CONDUCTING AIRBORNE TIME SPACING BASED
CONTINUOUS DESCENT ARRIVAL |
ICAS2012-10.8.3 |
| Balbo, M. |
TURBOJET ANALYTICAL MODEL
DEVELOPMENT AND VALIDATION |
ICAS2012-4.10.5 |
| Barber, T. J. |
PROGRESS IN UNDERSTANDING
TRANSONIC AND SUPERSONIC GROUND EFFECT AERODYNAMICS |
ICAS2012-10.6.3 |
| Baron, W. |
A PLANAR ANTENNA ARRAY
MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC |
ICAS2012-6.11.ST |
| Barriere, L. |
POSTBUCKLING COMPUTATION OF
LARGE STIFFENED STRUCTURES |
ICAS2012-8.1.3 |
| Barter, S. A. |
INVESTIGATION OF AN
IN-SERVICE CRACK SUBJECTED TO AERODYNAMIC BUFFET AND MANOEUVRE LOADS AND
EXPOSED TO AN CORROSIVE ENVIRONMENT |
ICAS2012-7.9.1 |
| Barth, J. E. |
STREAMWISE PORTHOLE FUEL
INJECTION FOR BOUNDARY-LAYER COMBUSTION INSIDE A SCRAMJET ENGINE |
ICAS 2012-P4.16 |
| Barthmes, S. |
NUMERICAL INVESTIGATION OF
THE EFFECT OF INFLOW DISTORTIONS ON TRANSONIC AXIAL COMPRESSOR STAGES WITH 2D
AND 3D CALCULATIONS |
ICAS2012-4.6.2 |
| Bartsch, M. |
NUMERICAL SIMULATIONS AND
EXPERIMENTAL INVESTIGATIONS ON QUASI-STATIC AND CYCLIC MIXED MODE
DELAMINATION OF MULTIDIRECTIONAL CFRP LAMINATES |
ICAS2012-7.4.2 |
| Basaglia, M. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
| Basov, V. N. |
FATIGUE DESIGN PROCEDURE OF
LONGITUDINAL AND TRANSVERSE FUSELAGE JOINTS |
ICAS2012-12.4.2 |
| Basset, P. -M. |
MODELING OF LOSS OF TAIL
ROTOR EFFECTIVENESS CONDUCTING TO UNANTICIPATED YAW |
ICAS2012-5.10.3 |
| Batten, D. |
ALTERNATIVE AVIATION FUEL
FEEDSTOCK: THE MICROALGAE SOLUTION? |
ICAS2012-8.6.2 |
| Baxley, B. T. |
INTERVAL MANAGEMENT WITH
SPACING TO PARALLEL DEPENDENT RUNWAYS (IMSPIDR) EXPERIMENT AND RESULTS |
ICAS2012-9.10.3 |
| Bayandor, J. |
DETAILED POST-SOFT IMPACT
PROGRESSIVE DAMAGE ANALYSIS FOR A HYBRID STRUCTURE JET ENGINE |
ICAS2012-4.2.3 |
| Bayandor, J. |
COUPLED
MICROMECHANICS-FINITE ELEMENT PROGRESSIVE FAILURE DYNAMIC ANALYSIS APPROACH:
F-16 CANOPY CASE STUDY |
ICAS2012-7.7.5 |
| Bayandor, J. |
REAL
TIME DIAGNOSIS OF DYNAMIC FAILURE IN FUTURE AEROSPACE STRUCTURES |
ICAS2012-8.11.2 |
| Bayandor, J. |
A
LEAP IN LEARNED BIO-INSPIRED FLIGHT |
ICAS2012-9.5.ST |
| Beaumier, P. |
NUMERICAL TOOLS DEVELOPED AT
ONERA FOR THE AERODYNAMIC ASSESSMENT OF PROPELLERS AND COUNTER-ROTATING OPEN
ROTORS |
ICAS2012-4.7.1 |
| Becker, R. -G. |
IMPACT OF ALTERNATIVE FUELS
ON ENGINE PERFORMANCE AND CO2-EMISSIONS |
ICAS2012-8.6.3 |
| Beguin, B. |
AERODYNAMIC OPTIMISATION OF
A MORPHING MEMBRANE WING |
ICAS2012-3.6.3 |
| Belo, E. M. |
AIRCRAFT EMERGENCY
EVACUATION SIMULATION USING ANT COLONY OPTIMIZATION |
ICAS2012-9.1.3 |
| Bendfeldt, P. |
EVALUATION OF CABIN
DISPLACEMENT VENTILATION UNDER FLIGHT CONDITIONS |
ICAS2012-6.10.2 |
| Benedictus, R. |
ENERGY DISTRIBUTION IN GLARE
AND 2024-T3 ALUMINIUM DURING LOW-VELOCITY IMPACT |
ICAS2012-7.7.2 |
| Berge, M. E. |
THE GENERALIZED ARRIVAL
PLANNER (GARP): MODELING AND ANALYSIS FOR ARRIVAL PLANNING |
ICAS2012-10.9.3 |
| Bergman, M. |
MORE ELECTRICAL
ENVIRONMENTAL CONTROL SYSTEM SIMULATION |
ICAS2012-6.6.4 |
| Berlowitz, I. |
CARGO FIRE PROTECTION
SYSTEMS FOR FREIGHTER CONVERSIONS |
ICAS2012-6.10.1 |
| Berry, P. |
RECYCLING OLD WEIGHT
ASSESSMENT METHODS AND GIVING THEM NEW LIFE IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS2012-1.1.2 |
| Berry, P. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
| Bertini, G. |
DESIGN ANALYSIS FOR HYBRID
PROPULSION |
ICAS2012-6.7.5 |
| Bertsch, L. |
FLIGHT TESTING OF NOISE
ABATING RNP PROCEDURES AND STEEP APPROACHES |
ICAS2012-4.9.1 |
| Bespalov, V. A. |
COMPUTATIONAL AND
EXPERIMENTAL RESEARCH OF BOLT JOINTS OF METAL AND COMPOSITE IN AIRFRAMES |
ICAS2012-8.4.ST |
| Bibel, G. |
BEYOND
THE BLACK BOX: THE FORENSICS OF AIRPLANE CRASHES |
ICAS2012-0.2 |
| Bil, C. |
METHODOLOGY FOR A
PRELIMINARY DESIGN STUDY OF A BOX-WING AIRLINER |
ICAS2012-1.10.3 |
| Bil, C. |
IMPROVEMENTS FOR OPTIMUM
PROFILE SCHEDULING OF USER PREFERRED TRAJECTORIES |
ICAS2012-10.3.2 |
| Blom, H. |
ANALYZING SEPARATION LOSS
EVENTS IN TWO-PAIRED AIRCRAFT TRAILING CONDUCTING AIRBORNE TIME SPACING BASED
CONTINUOUS DESCENT ARRIVAL |
ICAS2012-10.8.3 |
| Blondeau, C. |
AIRCRAFT CONCEPTUAL DESIGN
IN A MULTI-LEVEL, MULTI-FIDELITY, MULTI-DISCIPLINARY OPTIMIZATION PROCESS |
ICAS2012-1.6.4 |
| Blumrich, F. |
PARAMETRIC STUDY OF RAIM
PERFORMANCE USING NEARLY UNIFORMLY DISTRIBUTED REFERENCE POINTS ON THE
EARTH’S SURFACE |
ICAS2012-6.9.4 |
| Boblak, I. |
A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS2012-6.11.3 |
| Bock, M. |
IMPROVING THE PRODUCTION
QUALITY OF THE ADVANCED AUTOMATED FIBER PLACEMENT PROCESS BY MEANS OF ONLINE
PATH CORRECTION |
ICAS2012-6.1.3 |
| Böck, P. M. |
AIRPORT CAPACITY
REPRESENTATION BASED ON AIRSIDE SIMULATIONS |
ICAS2012-10.10.1 |
| Boehnke, D. |
MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS2012-6.4.1 |
| Böhnke, D. |
COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS2012-1.9.1 |
| Bojovschi, A. |
A PLANAR ANTENNA ARRAY
MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC |
ICAS2012-6.11.ST |
| Bolinches i-Gisbert, M. |
MODELLING OF A WARPING WING
FOR ENERGY CONSUMPTION MINIMIZATION |
ICAS2012-1.3.4 |
| Bolsunovsky, A. L. |
AN EXPERIENCE IN AERODYNAMIC
DESIGN OF TRANSPORT AIRCRAFT |
ICAS2012-2.9.3 |
| Bombardier, Y. |
PROBABILISTIC RISK ANALYSIS
FOR AIRCRAFT STRUCTURES WITH LIMITED IN-SERVICE DAMAGES |
ICAS2012-7.9.3 |
| Bondarenko, D. |
EXPERIMENTAL INVESTIGATIONS
OF HYDRAULIC DEVICES PERFORMANCE IN AVIATION ENGINE COMPARTMENT |
ICAS2012-P2.10 |
| Borello, F. |
VERY-LONG ENDURANCE SOLAR
POWERED AUTONOMOUS UAVS: ROLE AND CONSTRAINTS FOR GMES APPLICATIONS |
ICAS2012-4.7.5 |
| Borello, F. |
MORE/ALL ELECTRIC AIRCRAFT
BASED ON FUEL CELL ENERGY SYSTEM: THE ENFICA-FC EXPERIENCE |
ICAS2012-6.7.2 |
| Borovoy, V. |
NUMERICAL SIMULATION OF
THREE-DIMENSIONAL SHOCK-WAVE/BOUNDARY-LAYER INTERACTION ON SHARP AND BLUNTED
FLAT PLATE |
ICAS2012-2.4.2 |
| Bortholin, T. |
COMPUTATIONAL INVESTIGATION
OF ICING CONTAMINATION ON AIRFOIL |
ICAS2012-P2.19 |
| Bos, T. |
IMPLEMENTING TIME BASED CDA
OPERATIONS IN A MEDIUM-HIGH DENSITY ATM ENVIRONMENT |
ICAS2012-10.8.1 |
| Bosbach, J. |
EVALUATION OF CABIN
DISPLACEMENT VENTILATION UNDER FLIGHT CONDITIONS |
ICAS2012-6.10.2 |
| Bosnyakov, S. M. |
AN EXPERIENCE OF USING
NUMERICAL METHODS IN EXPERIMENTAL INVESTIGATIONS OF TsAGI |
ICAS2012-P2.6 |
| Bowcutt, K. |
HIFIRE: AN INTERNATIONAL COLLABORATION TO ADVANCE THE SCIENCE AND TECHNOLOGY OF HYPERSONIC FLIGHT |
ICAS2012-0.8 |
| Bowcutt, K. |
REAL
TIME DIAGNOSIS OF DYNAMIC FAILURE IN FUTURE AEROSPACE STRUCTURES |
ICAS2012-8.11.2 |
| Boyce, R. |
ROBUST DESIGN OPTIMIZATION
OF HIGH-PERFORMANCE AXISYMMETRIC SCRAMJETS BASED ON SURROGATE-ASSISTED
EVOLUTIONARY ALGORITHMS |
ICAS2012-4.11.3 |
| Boyce, R. B. |
NUMERICAL MODELLING OF
POROUS FUEL INJECTION IN A RADICAL FARMING SCRAMJET |
ICAS2012-4.11.1 |
| Boyce, R. B. |
JET INTERACTION IN A
HYPERSONIC FLOW: A COMPARISON BETWEEN PLIF THERMOMETRY AND COMPUTATIONAL
SIMULATION |
ICAS2012-4.11.2 |
| Boyce, R. R. |
THERMAL NON-EQUILIBRIUM
EFFECTS IN RADICAL FARMING SCRAMJETS |
ICAS2012-11.4.1 |
| Boykett, R. |
AGEING AIRCRAFT SYSTEMS
& COST EFFECTIVE SAFETY |
ICAS2012-12.3.2 |
| Boykett, R. |
QUANTITATIVE FRACTOGRAPHY
MARKERS FOR DETERMINING FATIGUE CRACK GROWTH RATES IN ALUMINIUM AND TITANIUM
AIRCRAFT STRUCTURES |
ICAS2012-12.4.1 |
| Bragin, A. A. |
DEVELOPMENT OF THE AUTOMATED
SYSTEM ON THE BASIS OF NEURAL NETWORKS FOR FLIGHT SAFETY OF AIRCRAFT |
ICAS2012-5.2.2 |
| Brandt, M. |
MICROSTRUCTURE AND
MECHANICAL PROPERTIES OF LASER CLADDING REPAIR OF AISI 4340 STEEL |
ICAS2012-12.4.4 |
| Braun, R. |
AIRCRAFT SYSTEM SIMULATION
FOR PRELIMINARY DESIGN |
ICAS2012-1.9.3 |
| Breitsamter, C. |
FLOW CHARACTERISTICS OF A
HELICOPTER FUSELAGE CONFIGURATION INCLUDING A ROTATING ROTOR HEAD |
ICAS2012-2.7.3 |
| Breitsamter, C. |
AERODYNAMIC OPTIMISATION OF
A MORPHING MEMBRANE WING |
ICAS2012-3.6.3 |
| Breitsamter, C. |
VORTEX FLOW MANIPULATION ON
GENERIC DELTA WING CONFIGURATIONS |
ICAS2012-3.6.4 |
| Breitsamter, C. |
AEROACOUSTIC ANALYSIS OF A
HELICOPTER CONFIGURATION WITH DUCTED TAIL ROTOR |
ICAS2012-3.9.1 |
| Brett, M. |
APPLICATION OF THE RANGE
SAFETY TEMPLATE TOOLKIT TO UAS RISK HAZARD ANALYSES SUPPORTING AIRWORTHINESS
REGULATION |
ICAS2012-9.2.3 |
| Brezillon, J. |
A FULLY AUTOMATED CAD-BASED
FRAMEWORK FOR SHAPE OPTIMIZATION |
ICAS2012-11.10.1 |
| Brezillon, J. |
NUMERICAL STUDY OF THE
REYNOLDS NUMBER EFFECT ON LOW ASPECT
RATIO WINGS AT LOW SPEED |
ICAS2012-2.10.2 |
| Briceno, S. I. |
A COMPETITIVE AND
REAL-OPTIONS FRAMEWORK FOR THE ECONOMIC ANALYSIS OF LARGE AEROSPACE PROGRAMS |
ICAS2012-6.3.2 |
| Brieschenk, S. |
NUMERICAL MODELLING OF
POROUS FUEL INJECTION IN A RADICAL FARMING SCRAMJET |
ICAS2012-4.11.1 |
| Brieschenk, S. |
JET INTERACTION IN A
HYPERSONIC FLOW: A COMPARISON BETWEEN PLIF THERMOMETRY AND COMPUTATIONAL
SIMULATION |
ICAS2012-4.11.2 |
| Brisbane Team, DSTO AVD |
HIFIRE-1 BOUNDARY-LAYER
TRANSITION MEASUREMENTS |
ICAS2012-3.10.3 |
| Brooks, L. A. |
EXPERIMENTAL INVESTIGATION
OF FLAT PLATE SELF-NOISE REDUCTION USING TRAILING EDGE SERRATIONS |
ICAS2012-9.11.1 |
| Brouwers, Y. H. A. |
THE DESIGN AND ENGINEERING
ENGINE. TOWARDS A MODULAR SYSTEM FOR COLLABORATIVE AIRCRAFT DESIGN |
ICAS2012-6.3.3 |
| Brown, L. J. |
EMERGING WIRELESS
TECHNOLOGIES TO IMPROVE AIRBORNE AVIATION SECURITY |
ICAS2012-9.6.2 |
| Brunello, D. |
NUMERICAL AND EXPERIMENTAL
ANALYSIS OF A REPRESENTATIVE ADF HELICOPTER FUSELAGE |
ICAS2012-2.7.2 |
| Brunet, M. |
THE EREA VISION ON HIGH
PRIORITY RESEARCH AXES TOWARDS AIR TRANSPORT SYSTEM 2050 |
ICAS2012-1.7.1 |
| Brunner, D. |
LAY-UP OPTIMIZATION OF
COMPOSITE PLATES TO DELAY MODE-JUMP INSTABILITIES |
ICAS2012-7.1.ST |
| Bueker, K. |
AN ASSET FOR IMPROVED
EFFICIENCY AND PUNCTUALITY IN AIR TRANSPORT |
ICAS2012-11.7.5 |
| Buisson, M. |
TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS2012-4.4.4 |
| Bukov, V. |
A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS2012-6.11.3 |
| Buzoverya, N. P. |
AN EXPERIENCE IN AERODYNAMIC
DESIGN OF TRANSPORT AIRCRAFT |
ICAS2012-2.9.3 |
| Buzuluk, V. I. |
ADVANCED AEROSPACE SYSTEMS
WITH INTERCONTINENTAL AND GLOBAL RANGE OF FLIGHT |
ICAS2012-1.5.2 |
| Cabut, A. |
FAULT DETECTION AND
RECONFIGURATION APPLIED TO A HELICOPTER SWASHPLATE ACTUATOR |
ICAS2012-5.1.2 |
| Cai, Y. |
THE PERFORMANCE COMPUTATION
OF THE HOT AIR ANTI-ICING SYSTEM OF AN AERO-ENGINE CONE |
ICAS2012-2.6.2 |
| Cairns, K. |
SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS2012-7.2.2 |
| Callantine, T. |
RESOLVING OFF-NOMINAL
SITUATIONS IN SCHEDULE-BASED TERMINAL AREA OPERATIONS: RESULTS FROM A
HUMAN-IN-THE-LOOP SIMULATION |
ICAS2012-10.5.2 |
| Callus, P. J. |
A PLANAR ANTENNA ARRAY
MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC |
ICAS2012-6.11.ST |
| Cambier, L. |
THE ONERA ELSA CFD SOFTWARE
: INPUT FROM RESEARCH AND FEEDBACK FROM INDUSTRY |
ICAS2012-2.1.1 |
| Campbell, D. |
A CAPABILITY FRAMEWORK FOR
MULTIPLE HETEROGENEOUS UAVS: FROM A MISSION COMMANDER'S PERSPECTIVE |
ICAS2012-9.7.3 |
| Campbell, D. A. |
THE AFFECT OF SCREEN SIZE ON
MISSION COMMANDER’S SITUATION AWARENESS |
ICAS2012-9.7.5 |
| Campos, L. M. B. C. |
A PROBABILITY ASSESSMENT OF
THE FLIGHT SAFETY RELEVANT TO COLLISION AVOIDANCE |
ICAS2012-10.7.5 |
| Campos, L. M. B. C. |
ON SOUND GENERATION BY
MOVING SURFACES AND CONVECTED SOURCES IN A FLOW |
ICAS2012-P2.8 |
| Campos, L. M. B. C. |
ANALYTICAL NATURAL
FREQUENCIES OF TAPERED WINGS |
ICAS2012-P3.2 |
| Canamar, A. |
ADVANCE SEAPLANE CONCEPTUAL
DESIGN ADAPTING TRIMARAN BOAT HULL CONCEPT |
ICAS2012-2.1.3 |
| Cao, X. |
A NEW APPROACH FOR RE-ENTRY
VEHICLE TRAJECTORY PLANNING AND GUIDANCE |
ICAS2012-5.7.5 |
| Cao, X. |
MANEUVERING TARGET TRACKING
BASED ON THE EKF |
ICAS2012-P5.2 |
| Capararo, D. |
FINITE ELEMENT SIMULATION OF
CRACK PROPAGATION IN MILITARY AIRCRAFT COATINGS |
ICAS2012-7.2.3 |
| Capra, B. R. |
NUMERICAL MODELLING OF
POROUS FUEL INJECTION IN A RADICAL FARMING SCRAMJET |
ICAS2012-4.11.1 |
| Capron, W. R. |
INTERVAL MANAGEMENT WITH
SPACING TO PARALLEL DEPENDENT RUNWAYS (IMSPIDR) EXPERIMENT AND RESULTS |
ICAS2012-9.10.3 |
| Carr, T. |
A NON-WEIGHT BASED,
MANUFACTURING INFLUENCED DESIGN (MIND) METHODOLOGY FOR PRELIMINARY DESIGN |
ICAS2012-6.4.3 |
| Carrier, G. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
| Carrier, G. |
AIRCRAFT CONCEPTUAL DESIGN
IN A MULTI-LEVEL, MULTI-FIDELITY, MULTI-DISCIPLINARY OPTIMIZATION PROCESS |
ICAS2012-1.6.4 |
| Carrier, G. |
AUTOMATED CHAIN FOR
AERODYNAMIC COMPUTATIONS MEETING AIRCRAFT TRIMMING REQUIREMENTS |
ICAS2012-2.10.1 |
| Castanie, B. |
POSTBUCKLING COMPUTATION OF
LARGE STIFFENED STRUCTURES |
ICAS2012-8.1.3 |
| Castanié, B. |
MODELLING OF IMPACT ON
SANDWICH STRUCTURE FOR FAST MAINTENANCE LOOPS |
ICAS2012-8.3.3 |
| Castelletti, L.-M. L. |
PRELIMINARY INVESTIGATION ON
THE FEASIBILITY OF A BIRD SURROGATE FOR FULL-SCALE BIRD IMPACT TEST |
ICAS2012-8.3.1 |
| Castillon, L. |
EVALUATION OF A MULTIPLE
FREQUENCY PHASE LAGGED METHOD FOR UNSTEADY NUMERICAL SIMULATIONS OF
MULTISTAGE TURBOMACHINERY |
ICAS2012-4.3.1 |
| Catalano, F. M. |
THE INFLUENCE OF DEMOISELLE
AIRCRAFT ON LIGHT AND GENERAL AVIATION DESIGN |
ICAS2012-1.7.ST |
| Catalano, F. M. |
AIRFOIL SELF NOISE REDUCTION
BY APPLICATION OF DIFFERENT TYPES OF TRAILING EDGE SERRATIONS |
ICAS2012-3.11.1 |
| Catalano, F. M. |
TRAILING EDGE TREATMENT TO
ENHANCE HIGH LIFT SYSTEM PERFORMANCE |
ICAS2012-3.2.3 |
| Catalano, F. M. |
WIND TUNNEL TESTING OF
POROUS DEVICES FOR THE REDUCTION OF FLAP SIDE-EDGE NOISE |
ICAS2012-9.11.2 |
| Catalano, F. M. |
COMPUTATIONAL INVESTIGATION
OF ICING CONTAMINATION ON AIRFOIL |
ICAS2012-P2.19 |
| Cattan, E. |
AEROELASTIC SIMULATION OF
FLEXIBLE FLAPPING WING BASED ON STRUCTURAL FEM AND QUASI-STEADY AERODYNAMIC
MODEL |
ICAS2012-8.5.1 |
| Cattaneo, G. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
| Cavagna, L. |
NEOCASS: AN OPEN SOURCE
ENVIRONMENT FOR THE AEROELASTIC ANALYSIS AT CONCEPTUAL DESIGN LEVEL |
ICAS2012-8.10.1 |
| Cazzato, L. |
PRELIMINARY DESIGN OF A
FUEL-CELL-BASED HYBRID-ELECTRICAL UAV |
ICAS2012-1.8.2 |
| Cecrdle, J. |
EIGENVALUE AND FLUTTER
SENSITIVITY ANALYSIS OF AIRLINER WING |
ICAS2012-P3.1 |
| Ceisel, J. |
A NON-WEIGHT BASED,
MANUFACTURING INFLUENCED DESIGN (MIND) METHODOLOGY FOR PRELIMINARY DESIGN |
ICAS2012-6.4.3 |
| Ceisel, J. |
A METHODOLOGY FOR PARAMETRIC
PRODUCTION PLANNING IN PRELIMINARY AIRCRAFT DESIGN |
ICAS2012-6.4.4 |
| Celikovsky, S. |
STABILIZATION OF
LONGITUDINAL AIRCRAFT MOTION USING MODEL PREDICTIVE CONTROL AND EXACT
LINEARIZATION |
ICAS2012-P5.11 |
| Ceron, E. D. |
TRAILING EDGE TREATMENT TO
ENHANCE HIGH LIFT SYSTEM PERFORMANCE |
ICAS2012-3.2.3 |
| Cervinka, J. |
WIND TUNNEL AND CFD STUDY OF
AIRFOIL WITH AIRBRAKE |
ICAS2012-10.6.ST1 |
| Cestino, E. |
VERY-LONG ENDURANCE SOLAR
POWERED AUTONOMOUS UAVS: ROLE AND CONSTRAINTS FOR GMES APPLICATIONS |
ICAS2012-4.7.5 |
| Cestino, E. |
MORE/ALL ELECTRIC AIRCRAFT
BASED ON FUEL CELL ENERGY SYSTEM: THE ENFICA-FC EXPERIENCE |
ICAS2012-6.7.2 |
| Chaboud, T. |
AUTOMATED CONFLICT-FREE
PLANNING: EXPERIMENTS ON REAL AIR TRAFFIC DATA |
ICAS2012-10.1.2 |
| Chaboud, T. |
MODELLING AIR TRAFFIC IMPACT
ON LOCAL AIR QUALITY WITH IESTA AND ADMS-AIRPORT: VALIDATION USING FIELD
MEASUREMENTS ON A REGIONAL AIRPORT |
ICAS2012-4.9.4 |
| Chai, J. |
TRANSONIC
DRAG REDUCTION ON A SUPERCRITICAL WING SECTION USING SHOCK CONTROL BUMPS |
ICAS2012-P2.3 |
| Chaitanya, M. V. R. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
| Chamberlain, J. |
CONCEPT OF INTEGRATION FOR
UAS OPERATIONS IN THE NAS |
ICAS2012-10.7.1 |
| Chandrasekhara, M. |
WATER TUNNEL FORCE AND
MOMENT STUDIES OF A MANEUVERING UCAV 1303 AND THEIR CONTROL |
ICAS2012-3.1.3 |
| Chang, C. W. T. |
EXPERIMENTAL INVESTIGATION
OF A BI-PLANE MICRO AIR VEHICLE |
ICAS2012-3.3.4 |
| Changenet, C. |
COUPLING MECH. & THERMAL
MODELS IN PRELIMINARY DESIGN OF POWER TRANSMISSIONS DRIVEN BY THERMAL ISSUES |
ICAS2012-6.6.1 |
| Chapelle, L. |
ASSESSMENT OF STRUCTURAL
EFFECT OF SELECTIVE STITCHING ON COMPOSITE SKIN-STIFFENER BONDING |
ICAS2012-8.9.1 |
| Chaplygin, V. |
COMPUTATIONAL AND
EXPERIMENTAL RESEARCH OF BOLT JOINTS OF METAL AND COMPOSITE IN AIRFRAMES |
ICAS2012-8.4.ST |
| Chassaing, J. -C. |
DERIVATED TURBULENCE MODEL
TO PREDICT HARMONIC LOADS IN TRANSONIC SEPARATED FLOWS OVER A BUMP |
ICAS2012-4.6.4 |
| Chassaing, P. |
MODELING OF THE INTERACTION
BETWEEN A TURBULENT FLOW AND AN ABLATABLE MATERIAL |
ICAS2012-3.8.2 |
| Che Idris, A. |
PERFORMANCE ANALYSIS OF A
SCRAMJET INLET-ISOLATOR USING EXPERIMENTAL & NUMERICAL METHODS |
ICAS2012-P4.12 |
| Che, B. |
IMPROVED EXACT STRIP
POSTBUCKLING ANALYSIS FOR ANISOTROPIC PLATES WITH FIXED, FREE AND STRAIGHT
EDGES |
ICAS2012-8.2.1 |
| Che, H. |
TRANSONIC
DRAG REDUCTION ON A SUPERCRITICAL WING SECTION USING SHOCK CONTROL BUMPS |
ICAS2012-P2.3 |
| Chedrik, V. |
ANALYSIS OF STATIC AND
DYNAMIC AEROELASTIC CHARACTERISTICS OF AIRPLANE IN TRANSONIC FLOW |
ICAS2012-8.10.4 |
| Chen, H. X. |
NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS2012-2.3.3 |
| Chen, J. |
RESEARCH ON AIRBORNE
INTELLIGENT HYDRAULIC PUMP SYSTEM |
ICAS2012-6.10.3 |
| Chen, N. |
UNCERTAINTY QUANTIFICATION
IN THE DEVELOPMENT OF AVIATION OPERATIONS TO REDUCE AVIATION EMISSIONS AND
CONTRAILS |
ICAS2012-7.10.2 |
| Chen, T. |
A CAPABILITY FRAMEWORK FOR
MULTIPLE HETEROGENEOUS UAVS: FROM A MISSION COMMANDER'S PERSPECTIVE |
ICAS2012-9.7.3 |
| Chen, T. |
PATH PLANNING FOR MULTI
HELICOPTER COORDINATED RESCUE |
ICAS2012-P8.5 |
| Chen, X. |
CONTROL ALLOCATION FOR
AIRCRAFTS WITH MULTIPLE CONTROL EFFECTORS DURING TAKEOFF AND LANDING PHASES |
ICAS2012-5.3.3 |
| Chen, Y. |
NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS2012-2.3.3 |
| Chen, Y. |
RESEARCH FOR JET FLOW INFLUENCES TO WING-MOUNTED CIVIL
AIRCRAFT AERODYNAMIC CHARACTERISTICS |
ICAS2012-2.9.1 |
| Chen, Z. |
NUMERICAL
SIMULATION OF BIRD-STRIKING PROCESS AND ITS EXPERIMENTAL VERIFICATION |
ICAS2012-8.9.4 |
| Cheng, H. |
INFORMATION THEORY APPLIED
TO A SELF-ORGANISED, UNMANNED AERIAL SYSTEM |
ICAS2012-11.7.4 |
| Cheng, J. -H. |
DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS2012-10.4.1 |
| Chernoray, V. |
MEASUREMENTS AND PREDICTION
OF LAMINAR-TURBULENT TRANSITION AT HIGH FREE-STREAM TURBULENCE & PRESSURE
GRADIENTS |
ICAS2012-3.10.5 |
| Chernov, A. V. |
STRENGTH CRITERIA
DEVELOPMENT FOR COMPOSITE STRUCTURES BASING ON SOLUTIONS SUPERPOSITION FOR
MODELS OF DIFFERENT LEVELS |
ICAS2012-7.1.2 |
| Chernov, A. V. |
INVESTIGATION OF CRACK
PROPAGATION BY OPTICAL INTERFEROMETRIC MEASUREMENTS OF LOCAL DEFORMATION
RESPONSE |
ICAS2012-7.9.2 |
| Chernyshov, V. |
A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS2012-6.11.3 |
| Chevagin, A. |
INTAKE CAPABILITY
IMPROVEMENTS IN RAMJET-TYPE PROPULSION SYSTEM |
ICAS2012-P4.3 |
| Chiesa, S. |
TURBOJET ANALYTICAL MODEL
DEVELOPMENT AND VALIDATION |
ICAS2012-4.10.5 |
| Chircop, K. |
A PROPOSAL FOR REVISED
APPROACHES AND PROCEDURES TO MALTA INTERNATIONAL AIRPORT |
ICAS2012-4.9.3 |
| Chircop, K. |
BI-OBJECTIVE PSEUDOSPECTRAL
OPTIMAL CONTROL TECHNIQUES FOR AIRCRAFT TRAJECTORY OPTIMIZATION |
ICAS2012-P5.6 |
| Cho, H. H. |
THERMAL ANALYSIS NEAR
SECONDARY INJECTION HOLE IN SITVC SYSTEM |
ICAS2012-P4.9 |
| Choi, B. |
EFFECT OF VENT MIXER TO
MIXING CHARACTERISTICS IN SUPERSONIC FLOW |
ICAS2012-P4.4 |
| Choi, H. |
VISION-BASED UAV GUIDANCE
AND ESTIMATION FOR AERIAL TARGET TRACKING |
ICAS2012-11.3.2 |
| Choi, H. -L. |
A PEG-BASED ASCENDING
GUIDANCE ALGORITHM FOR RAMJET-POWERED VEHICLES |
ICAS2012-5.7.4 |
| Christensen, S. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
| Chung, T. H. |
EXTENDING AUTONOMY
CAPABILITIES FOR UNMANNED SYSTEMS WITH CRUSER |
ICAS2012-11.6.3 |
| Ciampa, P.D. |
MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS2012-6.4.1 |
| Cikrikci, D. |
TOOL DEVELOPMENT FOR
AIRCRAFT LOADS POST-PROCESSING |
ICAS2012-P3.5 |
| Clark, G. |
MICROSTRUCTURE AND
MECHANICAL PROPERTIES OF LASER CLADDING REPAIR OF AISI 4340 STEEL |
ICAS2012-12.4.4 |
| Clarke, G. |
NUMERICAL AND EXPERIMENTAL
ANALYSIS OF A REPRESENTATIVE ADF HELICOPTER FUSELAGE |
ICAS2012-2.7.2 |
| Classen, A. B. |
AN ASSET FOR IMPROVED
EFFICIENCY AND PUNCTUALITY IN AIR TRANSPORT |
ICAS2012-11.7.5 |
| Clothier, R. A. |
THE SMART SKIES PROJECT:
ENABLING TECHNOLOGIES FOR FUTURE AIRSPACE ENVIRONMENTS |
ICAS2012-6.9.2 |
| Cockram, J. D. |
DEVELOPING THE USE OF
NEURAL-NETWORK TEST TECHNOLOGY FROM AVIONICS TO WIRING SYSTEMS |
ICAS2012-12.5.1 |
| Coldbeck, D. |
COMPOSITE SANDWICH PANEL
BIRDSTRIKE TESTING AND ANALYSIS |
ICAS2012-8.3.4 |
| Coman, F. |
FLOW-INDUCED FLUTTER OF
SLENDER CANTILEVER HIGH-COMPLIANCE PLATES |
ICAS2012-8.10.5 |
| Comendador, V. F. G. |
AIRCRAFT FLIGHT TRAJECTORY
DEVIATION IN THE STANDARD INSTRUMENT DEPARTURES. OPERATORS PENALTIES |
ICAS2012-10.10.2 |
| Conser, D. P. |
VIBRATION AND AEROELASTIC CLEARANCE WORK FOR JASSM INTEGRATION ONTO THE F/A-18A/B |
ICAS2012-8.10.3 |
| Consiglio, M. |
CONCEPT OF INTEGRATION FOR
UAS OPERATIONS IN THE NAS |
ICAS2012-10.7.1 |
| Cooper, M. A. |
TOWARDS TRAJECTORY
PREDICTION AND OPTIMISATION FOR ENERGY EFFICIENCY OF AN AIRCRAFT WITH
ELECTRICAL AND HYDRAULIC ACTUATION SYSTEMS |
ICAS2012-6.7.3 |
| Coporrella, M. |
EFFECT ON THE AERODYNAMIC
FORCING IN AN AXIAL TURBINE STAGE ON VARYING STATOR BLADE SHAPE |
ICAS2012-4.3.ST |
| Coppin, G. |
A CAPABILITY FRAMEWORK FOR
MULTIPLE HETEROGENEOUS UAVS: FROM A MISSION COMMANDER'S PERSPECTIVE |
ICAS2012-9.7.3 |
| Corcione, S. |
AERODYNAMIC ANALYSIS AND
DESIGN OF A TWIN-ENGINE COMMUTER
AIRCRAFT |
ICAS2012-1.6.2 |
| Corke, P. |
VISUAL SERVOING APPROACH TO
COLLISION AVOIDANCE FOR AIRCRAFT |
ICAS2012-11.3.1 |
| Correa, L. G. N. |
WIND TUNNEL TESTING OF
POROUS DEVICES FOR THE REDUCTION OF FLAP SIDE-EDGE NOISE |
ICAS2012-9.11.2 |
| Correale, G. |
NOVEL PASSIVE AND ACTIVE
FLOW CONTROL FOR HIGH LIFT |
ICAS2012-3.7.2 |
| Coughlan, P. |
BRISBANE AIRPORT'S NEW
PARALLEL RUNWAY |
ICAS2012-P8.4 |
| Crawford, B. R. |
INITIAL RESULTS FROM DSTO’S
CORROSION STRUCTURAL INTEGRITY ROADMAP |
ICAS2012-12.6.1 |
| Cresta, P. |
POSTBUCKLING COMPUTATION OF
LARGE STIFFENED STRUCTURES |
ICAS2012-8.1.3 |
| Crites, D. C. |
DEVELOPMENT OF AN
EXPERIMENTAL TECHNIQUE FOR HIGH TEMPERATURE IMPINGEMENT STUDIES |
ICAS2012-12.6.3 |
| Crossley, W. A. |
DEVELOPING OPTIMAL AIRLINE
FLEETS UNDER ENVIRONMENTAL AND CAPACITY CONSTRAINTS |
ICAS2012-7.10.1 |
| Crossley, W. A. |
MEASURING SYSTEM-WIDE
IMPACTS OF NEW AIRCRAFT ON THE ENVIRONMENT |
ICAS2012-7.11.1 |
| Crouse, G. L. |
ESTIMATING TIME TO LOSS OF
SEPARATION WITH UNCERTAIN POSITION AND VELOCITY MEASUREMENTS |
ICAS2012-10.7.4 |
| Crowther, W. |
TETHERING
UNMANNED ROTORCRAFT FOR HIGH-ENDURANCE OPERATIONS |
ICAS2012-P1.3 |
| Crump, M. |
ALL-SOURCE NAVIGATION FOR
ENHANCING UAV OPERATIONS IN GPS-DENIED ENVIRONMENTS |
ICAS2012-11.6.1 |
| Crump, M. |
INTELLIGENT LANDING SYSTEM
FOR LANDING UAVS AT UNSURVEYED AIRFIELDS |
ICAS2012-11.6.2 |
| Cuerno, C. |
LEGAL AND TECHNICAL
IMPLICATIONS OF THE SAFETY RECOMMENDATIONS ISSUED IN THE FINAL REPORTS OF THE
CIVIL AIR ACCIDENTS AND INCIDENTS INVESTIGATIONS |
ICAS2012-9.4.ST |
| Cuerno, C. |
PRELIMINARY AERODYNAMIC
INVESTIGATION OF AN UNMANNED BOX-WING AIRCRAFT |
ICAS2012-P2.13 |
| Cui, D. |
THE WORKFLOW CONSTRUCTION
AND MANAGEMENT IN AERONAUTICAL MULTIDISCIPLINARY OPTIMIZATION |
ICAS2012-2.1.2 |
| Cui, D. |
THE METHOD FOR NONLINEAR
ANALYSIS OPTIMIZATION IN AERONAUTICAL RESEARCH |
ICAS2012-P1.2 |
| Cui, R. H. |
RESEARCH ON CRACK GROWTH OF
MULTIPLE-SITE DAMAGED STRUCTURE |
ICAS2012-7.1.3 |
| Cuzieux, F. |
MODELING OF LOSS OF TAIL
ROTOR EFFECTIVENESS CONDUCTING TO UNANTICIPATED YAW |
ICAS2012-5.10.3 |
| da Silva, R. G. |
ON THE EFFECTS OF TURBULENCE
MODELING AND GRID REFINEMENT ON HIGH-LIFT CONFIGURATION AERODYNAMIC
SIMULATIONS |
ICAS2012-2.3.1 |
| Danilin, A. I. |
THE NEW OPTIMALITY CRITERIA
FOR STRUCTURAL DESIGN WITH CONSTRAINING ELASTIC DISPLACEMENTS |
ICAS2012-8.7.5 |
| Daoud, F. |
MULTIDISCIPLINARY AIRFRAME
DESIGN OPTIMIZATION |
ICAS2012-0.4 |
| David, M. |
IMPROVED DESIGN METHODS FOR
CRASHWORTHY COMPOSITE HELICOPTER STRUCTURES |
ICAS2012-8.1.2 |
| de Boer, A. |
THE EREA VISION ON HIGH
PRIORITY RESEARCH AXES TOWARDS AIR TRANSPORT SYSTEM 2050 |
ICAS2012-1.7.1 |
| de Boer, A. |
ACCELERATED LIFE CONSUMPTION
DUE TO THERMO-ACOUSTIC OSCILLATIONS IN GAS TURBINES: XFEM & CRACK |
ICAS2012-4.2.2 |
| De Crescenzio, F. |
INNOVATION IN MAN MACHINE
INTERFACES: USE OF 3D CONFORMAL SYMBOLS IN THE DESIGN OF FUTURE HUDS (HEAD UP
DISPLAYS) |
ICAS2012-9.7.2 |
| De felice, N. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
| De Gaspari, A. |
NEOCASS: AN OPEN SOURCE
ENVIRONMENT FOR THE AEROELASTIC ANALYSIS AT CONCEPTUAL DESIGN LEVEL |
ICAS2012-8.10.1 |
| de Lamberterie, P. |
COMPUTATIONAL ASPECTS OF
PROBABILISTIC ASSESSMENT OF UAS ROBUST AUTONOMY |
ICAS2012-9.2.2 |
| de Lamberterie, P. |
EVALUATION OF ROBUST
AUTONOMY AND IMPLICATIONS ON UAS DESIGN |
ICAS2012-9.4.2 |
| de Muynck, R. |
OPTIMIZING INBOUND AIRCRAFT
STREAMS USING AIRCRAFT DERIVED DATA AND RTA FUNCTIONALITY |
ICAS2012-10.4.4 |
| de Muynck, R. J. |
IMPLEMENTING TIME BASED CDA
OPERATIONS IN A MEDIUM-HIGH DENSITY ATM ENVIRONMENT |
ICAS2012-10.8.1 |
| de Olim, A. |
A PRACTICAL, ROUTE-BASED
APPROACH TO AIRSPACE CAPACITY MANAGEMENT |
ICAS2012-10.2.2 |
| De Saint Jean, M. |
STREAMWISE AND CROSSFLOW
INSTABILITIES ON INCLINED CIRCULAR CYLINDERS |
ICAS2012-3.10.2 |
| de Vries, H. |
EXPERIMENTAL/NUMERICAL
INVESTIGATION AIRFOIL WITH FLOW CONTROL BY SYNTHETIC JETS |
ICAS2012-3.7.5 |
| Dehne, T. |
EVALUATION OF CABIN
DISPLACEMENT VENTILATION UNDER FLIGHT CONDITIONS |
ICAS2012-6.10.2 |
| Deivasigamani, A. |
FLOW-INDUCED FLUTTER OF
SLENDER CANTILEVER HIGH-COMPLIANCE PLATES |
ICAS2012-8.10.5 |
| DeLaurentis, D. |
DESCRIPTION AND EVALUATION
OF MULTI-THREAT TRACKING ARCHITECTURES |
ICAS2012-11.2.3 |
| DeLaurentis, D. A. |
DEVELOPING OPTIMAL AIRLINE
FLEETS UNDER ENVIRONMENTAL AND CAPACITY CONSTRAINTS |
ICAS2012-7.10.1 |
| Della Vecchia, P. |
AERODYNAMIC ANALYSIS AND
DESIGN OF A TWIN-ENGINE COMMUTER
AIRCRAFT |
ICAS2012-1.6.2 |
| Delloue, D. |
COUPLING MECH. & THERMAL
MODELS IN PRELIMINARY DESIGN OF POWER TRANSMISSIONS DRIVEN BY THERMAL ISSUES |
ICAS2012-6.6.1 |
| Deng, J. |
DESIGN OF LAMINAR
SUPERCRITICAL AIRFOILS BASED ON NAVIER-STOKES EQUATIONS |
ICAS2012-2.2.2 |
| Dequand, S. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
| Derrien, J. -C. |
ELECTROMECHANICAL ACTUATOR
(EMA) ADVANCED TECHNOLOGIES FOR FLIGHT CONTROLS |
ICAS2012-6.8.ST |
| Desopper, A. |
MODELING OF LOSS OF TAIL
ROTOR EFFECTIVENESS CONDUCTING TO UNANTICIPATED YAW |
ICAS2012-5.10.3 |
| Desse, J. -M. |
SUBSONIC WAKE FLOWS ANALYSIS
BY DIGITAL THREE-WAVELENGTHS HOLOGRAPHIC INTERFEROMETRY |
ICAS2012-3.11.3 |
| Desyatnik, P. A. |
EFFECTS OF MANIPULATOR TYPE
AND FEEL SYSTEM CHARACTERISTICS ON HIGH-FREQUENCY BIODYNAMIC PILOT-AIRCRAFT
INTERACTION |
ICAS2012-5.9.3 |
| Desyatnik, P. A. |
SOME ASPECTS OF MOVING-BASE
SIMULATION OF UPSET RECOVERING MANEUVER |
ICAS2012-5.9.4 |
| Deutschmann, A. |
PREDICTION OF AIRPORT DELAYS
BASED ON NON-LINEAR CONSIDERATIONS OF AIRPORTS SYSTEMS |
ICAS2012-10.10.4 |
| Di Meo, G. A. |
INTEROPERABILITY OF MILITARY
AIRCRAFT VERSUS FUTURE AIR NAVIGATION SYSTEM (FANS) |
ICAS2012-10.1.3 |
| Dieke-Meier, F. |
THE NEED FOR A COLLISION
PREVENTION SYSTEM FOR THE PUSHBACK OF AIRCRAFT |
ICAS2012-9.10.5 |
| Djojodihardjo, H. |
CONCEPTUAL DESIGN AND AERODYNAMIC STUDY OF JOINED-WING
BUSINESS JET AIRCRAFT |
ICAS2012-1.10.4 |
| Djojodihardjo, H. |
CONCEPTUAL DESIGN AND
AERODYNAMIC STUDY OF BLENDED WING BODY BUSINESS JET |
ICAS2012-2.9.2 |
| Djojodihardjo, H. |
COMPUTATIONAL STUDY ON THE
INFLUENCE OF COANDA JET ON AIRFOILS: TWO-DIMENSIONAL CASE |
ICAS2012-4.6.ST2 |
| Doberstein, D. |
MODEL BASED DESIGN AND
EXPERIMENTAL VALIDATION OF ELECTRO-MECHANIC ACTUATOR SYSTEMS FOR A NOSE
LANDING GEAR |
ICAS2012-6.8.3 |
| Dobrev, Y. |
MODEL VALIDATION OF A
TILTWING UAV IN TRANSITION PHASE APPLYING WINDTUNNEL INVESTIGATIONS |
ICAS2012-11.1.1 |
| Dobrev, Y. |
CONTROL CONCEPT OF A
TILTWING UAV DURING LOW SPEED MANOEUVRING |
ICAS2012-11.1.2 |
| Doi, A. |
EXPERIMENTAL STUDY OF THE
MORPHING FLAP AS A LOW NOISE HIGH LIFT DEVICE FOR AIRCRAFT WING |
ICAS2012-9.11.3 |
| Doig, G. |
PROGRESS IN UNDERSTANDING
TRANSONIC AND SUPERSONIC GROUND EFFECT AERODYNAMICS |
ICAS2012-10.6.3 |
| Döll, C. |
AUTOPILOT
DESIGN FOR THE EOLE DEMONSTRATOR |
ICAS2012-5.3.4 |
| Dolvin, D. J. |
HIFIRE: AN INTERNATIONAL COLLABORATION TO ADVANCE THE SCIENCE AND TECHNOLOGY OF HYPERSONIC FLIGHT |
ICAS2012-0.8 |
| Dong, W. |
THE PERFORMANCE COMPUTATION
OF THE HOT AIR ANTI-ICING SYSTEM OF AN AERO-ENGINE CONE |
ICAS2012-2.6.2 |
| Dong, W. F. |
DETERMINATION OF AIRBORNE
RECORDED PARAMETERS FOR COMPREHENSIVE FLIGHT DATA MONITORING PROGRAM |
ICAS2012-9.4.1 |
| Dong, Y. |
RESEARCH ON ESTIMATING
METHOD OF FUEL AND EMISSIONS USING NEURAL NETWORKS IN LTO CYCLE FOR
PRELIMINARY AIRCRAFT DESIGN |
ICAS2012-7.11.2 |
| Donough, M. J. |
CRITICAL ASSESSMENT OF
FAILURE CRITERION FOR ADHESIVELY BONDED COMPOSITE JOINT REPAIR DESIGN |
ICAS2012-12.2.2 |
| Doolan, C. J. |
EXPERIMENTAL INVESTIGATION
OF FLAT PLATE SELF-NOISE REDUCTION USING TRAILING EDGE SERRATIONS |
ICAS2012-9.11.1 |
| Dorbath, F. |
A KNOWLEDGE BASED APPROACH
FOR EXTENDED PHYSICS-BASED WING MASS ESTIMATION IN EARLY DESIGN STAGES |
ICAS2012-1.1.1 |
| Dragan, K. |
FATIGUE LIFE ANALYSIS OF
MAIN LANDING GEAR PULL-ROD OF THE
FIGHTER JET AIRCRAFT |
ICAS2012-12.4.3 |
| Dridi, W. |
MULTI-OBJECTIVE OPTIMIZATION
OF MULTI-ELEMENT HIGH-LIFT AIRFOIL |
ICAS2012-2.3.4 |
| Drobik, J. |
A RECENT HISTORY OF THE
EVOLUTION OF AUSTRALIA’S AERODYNAMICS STORE SEPARATION CAPABILITY – THROUGH
INDIGENOUS AND INTERNATIONAL PROGRAMS |
ICAS2012-10.6.4 |
| Du, H. |
THE WORKFLOW CONSTRUCTION
AND MANAGEMENT IN AERONAUTICAL MULTIDISCIPLINARY OPTIMIZATION |
ICAS2012-2.1.2 |
| Du, H. |
THE METHOD FOR NONLINEAR
ANALYSIS OPTIMIZATION IN AERONAUTICAL RESEARCH |
ICAS2012-P1.2 |
| Duan, Z. W. |
INVESTIGATION OF PASSIVE
FLOW CONTROL METHODOLOGIES USING SST-IDDES |
ICAS2012-P2.7 |
| Dubinsky, V. |
OUTLINE OF AIRCRAFT
STRUCTURE HEALTH AND USAGE MONITORING SYSTEMS AND METHODS USED FOR THEIR
REALIZATIONS |
ICAS2012-12.1.2 |
| Dubois, J. |
SIMULATION OF THE FULL
COUPLING BETWEEN THE RADIATION TRANSFER AND THE AERODYNAMICS FOR HYPERSONIC REENTRY PROBES |
ICAS2012-3.8.ST |
| Dubovikov, E. |
NOVEL APPROACH AND ALGORITHM
FOR SEARCHING RATIONAL NONCONVENTIONAL AIRFRAME CONCEPTS OF NEW GENERATION
AIRCRAFTS |
ICAS2012-8.8.2 |
| Dubovitskiy, A. |
EXPERIMENTAL INVESTIGATIONS
OF HYDRAULIC DEVICES PERFORMANCE IN AVIATION ENGINE COMPARTMENT |
ICAS2012-P2.10 |
| Duda, H. |
FLIGHT PERFORMANCE OF
LIGHTWEIGHT GYROPLANES |
ICAS2012-5.6.2 |
| Duong, C. G. |
PILOT CONVECTIVE WEATHER
DECISION MAKING IN EN ROUTE AIRSPACE |
ICAS2012-10.4.3 |
| Dutré, S. |
IDENTIFICATION OF HELICOPTER
GROUND RESONANCE WITH MULTI-BODY SIMULATION |
ICAS2012-8.3.2 |
| Dzikus, N. |
TECHNOLOGY ASSESSMENT OF
FUTURE AIRCRAFT: SOCIO-ECO-EFFICIENCY IN CONCEPTUAL AIRCRAFT DESIGN |
ICAS2012-1.9.2 |
| Dzuba, A. S. |
INVESTIGATION OF CRACK
PROPAGATION BY OPTICAL INTERFEROMETRIC MEASUREMENTS OF LOCAL DEFORMATION
RESPONSE |
ICAS2012-7.9.2 |
| Efremov, A. V. |
TECHNIQUE FOR FLYING
QUALITIES AND PIO PREDICTION |
ICAS2012-5.9.2 |
| Eggers and the Shefex II-Team, T. |
THE SHEFEX II EXPERIMENTAL
RE-ENTRY VEHICLE: PRESENTATION OF FLIGHT TEST RESULTS |
ICAS2012-5.4.4 |
| Eggers, T. |
NUMERICAL INVESTIGATION ON
THE POTENTIAL OF STEAM COOLING FOR THE SKYLON SPACEPLANE IN HYPERSONIC FLOW |
ICAS2012-2.8.1 |
| Egorov, I. |
NUMERICAL SIMULATION OF
THREE-DIMENSIONAL SHOCK-WAVE/BOUNDARY-LAYER INTERACTION ON SHARP AND BLUNTED
FLAT PLATE |
ICAS2012-2.4.2 |
| Ehmer, H. |
ICAO’S BALANCED APPROACH TO
NOISE MANAGEMENT AND ITS INFLUENCE ON THE ECONOMIC IMPACT OF AIR
TRANSPORTATION |
ICAS2012-7.10.4 |
| Eitelberg, G. |
PROPELLER INDUCED GROUND
VORTEX |
ICAS2012-4.10.3 |
| Ekhtiari, M. |
WAVELET-BASED ACTIVE SENSING
FOR QUANTITATIVE ASSESSMENT OF THROUGH-THICKNESS CRACK SIZE AND ANGLE IN
COMPOSITE PLATES |
ICAS2012-P3.8 |
| Ellbrant, L. |
CFD OPTIMIZATION OF A
TRANSONIC COMPRESSOR USING MULTIOBJECTIVE GA AND METAMODELS |
ICAS2012-4.6.3 |
| Ellström, H. |
MORE ELECTRICAL
ENVIRONMENTAL CONTROL SYSTEM SIMULATION |
ICAS2012-6.6.4 |
| Elston, J. |
SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS2012-7.2.2 |
| Enea, G. |
A COMPARISON OF
4D-TRAJECTORY OPERATIONS ENVISIONED FOR 'NEXTGEN' AND 'SESAR', SOME
PRELIMINARY FINDINGS |
ICAS2012-10.3.1 |
| Enqvist, M. |
NONLINEAR AERODYNAMIC
MODELING OF UNSTABLE AIRCRAFT USING FLIGHT TEST DATA |
ICAS2012-5.10.1 |
| Entzinger, J. O. |
INSIDE THE PILOTS MIND:
VISUAL INFORMATION USE IN MANUAL AIRCRAFT LANDINGS |
ICAS2012-9.7.1 |
| Erdelyi, H. |
DESIGN STUDY OF AN ACTIVE
GURNEY FLAP SYSTEM FOR HELICOPTER ROTOR BLADES |
ICAS2012-6.11.1 |
| Erdem, E. |
PERFORMANCE ANALYSIS OF A
SCRAMJET INLET-ISOLATOR USING EXPERIMENTAL & NUMERICAL METHODS |
ICAS2012-P4.12 |
| Eriksson, B. |
AIRCRAFT SYSTEM SIMULATION
FOR PRELIMINARY DESIGN |
ICAS2012-1.9.3 |
| Eriksson, L. -E. |
CFD OPTIMIZATION OF A
TRANSONIC COMPRESSOR USING MULTIOBJECTIVE GA AND METAMODELS |
ICAS2012-4.6.3 |
| Erlandsson, T. |
AUTOMATION GUIDELINES FOR
INTRODUCING SURVIVABILITY ANALYSIS IN FUTURE FIGHTER AIRCRAFT |
ICAS2012-9.1.1 |
| Everdij, M. |
ANALYZING SEPARATION LOSS
EVENTS IN TWO-PAIRED AIRCRAFT TRAILING CONDUCTING AIRBORNE TIME SPACING BASED
CONTINUOUS DESCENT ARRIVAL |
ICAS2012-10.8.3 |
| Faggiani, A. |
LAY-UP OPTIMIZATION OF
COMPOSITE PLATES TO DELAY MODE-JUMP INSTABILITIES |
ICAS2012-7.1.ST |
| Falzon, B. G. |
LAY-UP OPTIMIZATION OF
COMPOSITE PLATES TO DELAY MODE-JUMP INSTABILITIES |
ICAS2012-7.1.ST |
| Falzon, B. G. |
AN INVESTIGATION OF MODE I
FRACTURE TOUGHNESS USING ALIGNED CARBON-NANOTUBE FORESTS AT THE CRACK
INTERFACE |
ICAS2012-7.3.2 |
| Fateev, V. A. |
EXPERIMENTAL AND NUMERICAL
STUDY OF TWO FIRST HIGHLY-LOADED STAGES OF COMPRESSORS AS A PART OF HPC AND
SEPARATE UNIT |
ICAS2012-4.6.1 |
| Faugere, E. |
COUPLING MECH. & THERMAL
MODELS IN PRELIMINARY DESIGN OF POWER TRANSMISSIONS DRIVEN BY THERMAL ISSUES |
ICAS2012-6.6.1 |
| Featherston, C. |
IMPROVED EXACT STRIP
POSTBUCKLING ANALYSIS FOR ANISOTROPIC PLATES WITH FIXED, FREE AND STRAIGHT
EDGES |
ICAS2012-8.2.1 |
| Fedina, Y. A. |
VIBRATION STRENGTH INCREASE
OF ROTATING BLADES USING DYNAMIC SPIN RIGS |
ICAS2012-12.6.4 |
| Feih, S. |
DAMAGE TOLERANCE OF Z-PINNED
COMPOSITE JOINTS |
ICAS2012-7.5.2 |
| Feng, W. -C. |
A NEW METHOD OF CALCULATION
THE DELAY TIME OF MULTI-CREW MEMBER EJECTION |
ICAS2012-P6.2 |
| Ferrand, P. |
TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS2012-4.4.4 |
| Ferrand, P. |
DERIVATED TURBULENCE MODEL
TO PREDICT HARMONIC LOADS IN TRANSONIC SEPARATED FLOWS OVER A BUMP |
ICAS2012-4.6.4 |
| Ferreira, L. O. F. |
AIRCRAFT EMERGENCY
EVACUATION SIMULATION USING ANT COLONY OPTIMIZATION |
ICAS2012-9.1.3 |
| Feuerle, T. |
GBAS CURVED APPROACH
PROCEDURES: ADVANTAGES, CHALLENGES AND APPLICABILITY |
ICAS2012-4.9.2 |
| Fezans, N. |
EMERGENCY PROPULSION-BASED
AUTOLAND SYSTEM |
ICAS2012-5.1.3 |
| Fezans, N. |
A MODEL OF HORIZONTAL
TAILPLANE DAMAGE FOR USE IN FLIGHT DYNAMICS |
ICAS2012-P5.3 |
| Fielding, J. P. |
BOX WING AIRCRAFT CONCEPTUAL
DESIGN |
ICAS2012-1.9.ST |
| Fielding, J. P. |
PRELIMINARY STUDY OF EMA
LANDING GEAR ACTUATION |
ICAS2012-6.8.2 |
| Figat, M. |
MODULAR AEROPLANE SYSTEM. A
CONCEPT AND INITIAL INVESTIGATION |
ICAS2012-1.3.2 |
| Filippis, L. De |
AN INNOVATIVE MISSION
MANAGEMENT SYSTEM FOR FIXED-WING UAVS |
ICAS2012-11.7.1 |
| Filsinger, J. |
ASSESSMENT OF STRUCTURAL
EFFECT OF SELECTIVE STITCHING ON COMPOSITE SKIN-STIFFENER BONDING |
ICAS2012-8.9.1 |
| Fischer, M. |
ARTIFICIAL HINGED-WING
BIRD WITH ACTIVE TORSION AND PARTIALLY
LINEAR KINEMATICS |
ICAS2012-3.6.1 |
| Fisher, A. |
DYNAMIC SURFACE PRESSURE
MEASUREMENTS ON A FLAPPING WING IN SMOOTH AND TURBULENT FLOW |
ICAS2012-9.11.ST1 |
| Fitzpatrick, I. R. |
DESIGN OF COMPOSITE
STRUCTURES FOR IMPROVED AEROELASTIC PERFORMANCE |
ICAS2012-8.4.4 |
| Foenander, J. J. |
DESIGN
OF A TWO-DIMENSIONAL GASDYNAMIC NOZZLE USING MULTI-OBJECTIVE PARTICLE SWARM
OPTIMISATION |
ICAS2012-P4.8 |
| Fomin, V. |
DESIGNING PRO-COMPOSITE
AIRCRAFT CONCEPTS AND LAYOUTS TO MAXIMIZE POTENTIAL BENEFITS OF HIGH SPECIFIC
STRENGTH OF CFRP |
ICAS2012-1.7.3 |
| Fomin, V. P. |
STRENGTH CRITERIA
DEVELOPMENT FOR COMPOSITE STRUCTURES BASING ON SOLUTIONS SUPERPOSITION FOR
MODELS OF DIFFERENT LEVELS |
ICAS2012-7.1.2 |
| Foong, K. E. |
CONCEPTUAL DESIGN AND AERODYNAMIC STUDY OF JOINED-WING
BUSINESS JET AIRCRAFT |
ICAS2012-1.10.4 |
| Ford, J. J |
DESIGN OF FLIGHT AVOIDANCE
MANOEUVRE ALPHABETS FOR MIXED CENTRALISED-DECENTRALISED SEPARATION MANAGEMENT |
ICAS2012-10.7.3 |
| Ford, J. J. |
FLIGHT TRIAL OF AN
ELECTRO-OPTICAL SENSE-AND-AVOID SYSTEM |
ICAS2012-11.2.1 |
| Ford, J. J. |
FIELD-OF-VIEW, DETECTION
RANGE, AND FALSE ALARM TRADE-OFFS IN VISION-BASED AIRCRAFT DETECTION |
ICAS2012-6.9.1 |
| Forrester, A. J. |
MODELLING OF A WARPING WING
FOR ENERGY CONSUMPTION MINIMIZATION |
ICAS2012-1.3.4 |
| Forslund, A. |
ROBUST LIFECYCLE
OPTIMIZATION OF TURBINE COMPONENTS USING SIMULATION PLATFORMS |
ICAS2012-4.3.2 |
| Fosso-Pouangue, A. |
MULTI-OBJECTIVE OPTIMIZATION
OF MULTI-ELEMENT HIGH-LIFT AIRFOIL |
ICAS2012-2.3.4 |
| Francia, D. |
DESIGN ANALYSIS FOR HYBRID
PROPULSION |
ICAS2012-6.7.5 |
| Francia, D. |
A
META-HEURISTIC APPROACH TO SIMULATE TAXI OPERATIONS |
ICAS2012-P8.7 |
| Fransson, T. |
DERIVATED TURBULENCE MODEL
TO PREDICT HARMONIC LOADS IN TRANSONIC SEPARATED FLOWS OVER A BUMP |
ICAS2012-4.6.4 |
| Freeman, D. |
METHODOLOGY FOR THE DESIGN
OF UNMANNED AIRCRAFT PRODUCT FAMILIES |
ICAS2012-9.9.2 |
| Freeman, D. |
DESIGN OF UNMANNED AIR
SYSTEMS FOR USE IN SEARCH AND RESCUE IN THE NORTH ATLANTIC |
ICAS2012-9.9.3 |
| Fricke, H. |
DYNAMIC TURNAROUND
MANAGEMENT IN A HIGHLY AUTOMATED AIRPORT ENVIRONMENT |
ICAS2012-10.9.2 |
| Fricke, H. |
THE NEED FOR A COLLISION
PREVENTION SYSTEM FOR THE PUSHBACK OF AIRCRAFT |
ICAS2012-9.10.5 |
| Fricke, H. |
INVESTIGATING THE SAFETY
IMPACT OF TIME BUFFERS IN CURRENT TMA ARRIVAL OPERATIONS |
ICAS2012-9.4.3 |
| Friswell, M. I. |
COMPUTATIONAL AND
EXPERIMENTAL ANALYSIS OF THE ACTIVE MORPHING WING CONCEPT |
ICAS2012-2.5.3 |
| Frousheger, D. |
THE SMART SKIES PROJECT:
ENABLING TECHNOLOGIES FOR FUTURE AIRSPACE ENVIRONMENTS |
ICAS2012-6.9.2 |
| Fu, S. |
NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS2012-2.3.3 |
| Fu, S. |
INVESTIGATION OF PASSIVE
FLOW CONTROL METHODOLOGIES USING SST-IDDES |
ICAS2012-P2.7 |
| Fu, W. |
INVESTIGATION
ON PROPELLER ENGINE OPTIMUM INSTALLATION POSITION ON A SOLAR POWERED UNMANNED
AERIAL VEHICLE |
ICAS2012-2.10.5 |
| Fu, W. |
EXPLORING
THE AERODYNAMIC INTERFERENCE OF PROPELLER-WING ON A SOLAR POWERED UNMANNED
AERIAL VEHICLE |
ICAS2012-9.8.3 |
| Fu, Y. L |
A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
| Fu, Y. L. |
INVESTIGATION IN THE DYNAMIC
FORCE EQUALIZATION OF DISSIMILAR REDUNDANT ACTUATION SYSTEMS OPERATING IN
ACTIVE/ACTIVE MODE |
ICAS2012-6.8.1 |
| Fucke, L. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
| Fucke, L. |
UNRELIABLE AIRSPEED – MAKING
VALID ASSUMPTIONS ON FLIGHT CREW PERFORMANCE |
ICAS2012-9.3.4 |
| Fujimori, A. |
ESTIMATION OF AERODYNAMIC
DERIVATIVES IN AIRCRAFT MODEL USING ITERATIVE LEARNING IDENTIFICATION |
ICAS2012-5.10.5 |
| Fujishiro, T. |
INVESTIGATION ON STRUCTURAL
AND AERODYNAMIC CHARACTERISTICS OF RESONANT TYPE ELASTIC FLAPPING WING |
ICAS2012-9.5.3 |
| Fujita, K. |
EVALUATION OF DYNAMIC
BEHAVIOR OF A DEPLOYABLE WING UAV BY DROP TEST |
ICAS2012-P2.20 |
| Fujiwara, K. |
TITANIUM METAL MATRIX
COMPOSITE DEVELOPMENT FOR COMMERCIAL AIRCRAFT LANDING GEAR STRUCTURE |
ICAS2012-7.5.1 |
| Fukuda, Y. |
CONTINUOUS DESCENT
TRAJECTORY WITH OPTIMUM ARRIVAL TIME CONTROLLABILITY |
ICAS2012-P8.3 |
| Fukuoka, K. |
FUNDAMENTAL CHARACTERISTICS
OF DECENTRALIZED AIR TRAFFIC FLOW CONTROL IN HIGH DENSITY CORRIDOR |
ICAS2012-10.7.2 |
| Fukushima, Y. |
ESTIMATION OF NOISE
SHIELDING EFFECT OF NEXT-GENERATION AIRCRAFT BY A COMPUTATIONAL AEROACOUSTICS
METHOD |
ICAS2012-3.9.2 |
| Funabiki, K. |
EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS2012-9.3.1 |
| Gaffuri, M. |
NUMERICAL STUDY OF THE
REYNOLDS NUMBER EFFECT ON LOW ASPECT
RATIO WINGS AT LOW SPEED |
ICAS2012-2.10.2 |
| Gaind, R. |
AN EXPERIMENTAL STUDY OF A
PULSED AIR JET AND AN ACOUSTIC SYNTHETIC JET ON A LOW SPEED TURBULENT
BOUNDARY LAYER |
ICAS2012-3.5.1 |
| Galea, S. |
PROBING THE LIMITS - NEW
OPPORTUNITIES IN THERMOELASTIC STRESS ANALYSIS |
ICAS2012-12.1.1 |
| Galea, S. C. |
BI-AXIAL VIBRATION ENERGY
HARVESTING FOR USE ON AEROSPACE PLATFORMS |
ICAS2012-6.7.1 |
| Galinski, C. |
MODULAR AEROPLANE SYSTEM. A
CONCEPT AND INITIAL INVESTIGATION |
ICAS2012-1.3.2 |
| Galinski, C. |
RESULTS OF THE GUST
RESISTANT MAV PROGRAMME |
ICAS2012-3.1.1 |
| Gallego, J. M. |
LEGAL AND TECHNICAL
IMPLICATIONS OF THE SAFETY RECOMMENDATIONS ISSUED IN THE FINAL REPORTS OF THE
CIVIL AIR ACCIDENTS AND INCIDENTS INVESTIGATIONS |
ICAS2012-9.4.ST |
| Gamaleri, M. |
EMERGENCY PROPULSION-BASED
AUTOLAND SYSTEM |
ICAS2012-5.1.3 |
| Gao, Z. |
WING-BODY OPTIMIZATION BASED
ON MULTI-FIDELITY SURROGATE MODEL |
ICAS2012-11.10.5 |
| Gao, Z. |
EXTENSIONS OF MENTER’S SST
TRANSITION MODEL TO SIMULATE HYPERSONIC AND CROSS-FLOW TRANSITION |
ICAS2012-11.4.ST |
| Gao, Z. |
APPLICATION
OF TWO TRANSITION MODELS TO FLOWS AROUND AIRFOILS |
ICAS2012-2.4.4 |
| Gao, Z. |
CONTROL ALLOCATION FOR
AIRCRAFTS WITH MULTIPLE CONTROL EFFECTORS DURING TAKEOFF AND LANDING PHASES |
ICAS2012-5.3.3 |
| Gao, Z. H. |
STUDY
ON MODELING PILOT BEHAVIOR BY ARTIFICIAL NEURAL NETWORK |
ICAS2012-5.9.ST |
| Gao, Z. -H. |
NUMERICAL SIMULATION OF
TRANSONIC SHOCK-VORTEX INTERACTION FLOW AROUND THE VFE-2 DELTA WING BASED ON
MDDES |
ICAS2012-P2.4 |
| Garcia, E. |
METHODOLOGY FOR THE DESIGN
OF UNMANNED AIRCRAFT PRODUCT FAMILIES |
ICAS2012-9.9.2 |
| Garcia, E. |
DESIGN OF UNMANNED AIR
SYSTEMS FOR USE IN SEARCH AND RESCUE IN THE NORTH ATLANTIC |
ICAS2012-9.9.3 |
| Garcia, E. |
EVALUATING FLEXIBILITY IN
AIRPORT CAPACITY-ENHANCING TECHNOLOGY INVESTMENTS |
ICAS2012-P8.2 |
| García, E. |
HALA!: TOWARDS HIGHER LEVELS
OF AUTOMATION IN ATM. POSITION PAPER -STATE OF THE ART AND RESEARCH AGENDA |
ICAS2012-10.1.1 |
| García, E. |
AIRCRAFT FLIGHT TRAJECTORY
DEVIATION IN THE STANDARD INSTRUMENT DEPARTURES. OPERATORS PENALTIES |
ICAS2012-10.10.2 |
| Gareev, A. M. |
MODELING OF FLUID CONDITION
OF AIRCRAFT HYDRAULIC SYSTEM |
ICAS2012-6.6.2 |
| Gareyev, T. M. |
MODELING OF FLUID CONDITION
OF AIRCRAFT HYDRAULIC SYSTEM |
ICAS2012-6.6.2 |
| Garrett, S. J. |
STREAMWISE AND CROSSFLOW
INSTABILITIES ON INCLINED CIRCULAR CYLINDERS |
ICAS2012-3.10.2 |
| Garrett, S. J. |
ON THE EFFECT OF DISTRIBUTED
ROUGHNESS ON TRANSITION OVER ROTOR-STATOR DEVICES |
ICAS2012-3.10.4 |
| Garry, K. P. |
TIME DEPENDENT ANALYSIS OF A
RECTANGULAR SYNTHETIC JET |
ICAS2012-3.7.1 |
| Gauci, J. |
CORRESPONDENCE AND
CLUSTERING METHODS FOR IMAGE-BASED WING-TIP COLLISION AVOIDANCE TECHNIQUES |
ICAS2012-9.10.4 |
| Geesing, I. J. A. K. |
EXPERIMENTAL/NUMERICAL
INVESTIGATION AIRFOIL WITH FLOW CONTROL BY SYNTHETIC JETS |
ICAS2012-3.7.5 |
| Gehre, R. M. |
THERMAL NON-EQUILIBRIUM
EFFECTS IN RADICAL FARMING SCRAMJETS |
ICAS2012-11.4.1 |
| Gehre, R. M. |
JET INTERACTION IN A
HYPERSONIC FLOW: A COMPARISON BETWEEN PLIF THERMOMETRY AND COMPUTATIONAL
SIMULATION |
ICAS2012-4.11.2 |
| Gehri, A. |
SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS2012-10.6.1 |
| George, G. |
FINITE ELEMENT SIMULATION OF
CRACK PROPAGATION IN MILITARY AIRCRAFT COATINGS |
ICAS2012-7.2.3 |
| Gerardo Castro, M. P. |
MULTIDISCIPLINARY DESIGN AND
FLIGHT TESTING OF A REMOTE GAS/PARTICLE AIRBORNE SENSOR SYSTEM |
ICAS2012-6.10.4 |
| Ghadiri, B. |
NONLINEAR AEROELASTIC
ANALYSIS OF SWEPT WINGS IN COMPRESSIBLE FLOW VIA THE HARMONIC BALANCE METHOD |
ICAS2012-8.7.1 |
| Ghorbani, K. |
A PLANAR ANTENNA ARRAY
MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC |
ICAS2012-6.11.ST |
| Giacobello, M. |
NUMERICAL STUDY ON THE
EFFECT OF VARYING SPANWISE TWIST ON LOW-REYNOLDS-NUMBER FLAPPING FLIGHT |
ICAS2012-2.5.1 |
| Gibbon, R. |
COMPOSITE SANDWICH PANEL
BIRDSTRIKE TESTING AND ANALYSIS |
ICAS2012-8.3.4 |
| Gires, E. |
PERFORMANCE TEST OF A
SMALL-SCALE TURBOJET ENGINE RUNNING ON A PALM OIL BIODIESEL - JET A BLEND |
ICAS2012-4.8.1 |
| Gluchshenko, O. |
OPTIMIZATION OF RUNWAY
CAPACITY UTILIZATION IN THE CASE OF GENERAL PARETO CURVE |
ICAS2012-10.3.4 |
| Go, T. H. |
FLEXIBLE WING AERODYNAMICS
AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.1 |
| Go, T. H. |
EXPERIMENTAL INVESTIGATION
OF A BI-PLANE MICRO AIR VEHICLE |
ICAS2012-3.3.4 |
| Goda, Y. |
EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS2012-9.3.1 |
| Goetzendorf-Grabowski, T. G. |
MADO – SOFTWARE PACKAGE FOR
HIGH ORDER MULTIDISCIPLINARY AIRCRAFT
DESIGN AND OPTIMIZATION |
ICAS2012-1.9.4 |
| Goizueta, N. G. |
AN EXPERIMENTAL AND
NUMERICAL STUDY OF THE EFFECT OF NOSE BLUNTING ON A CONICAL NOSED BODY AT
TRANSONIC SPEED |
ICAS2012-2.8.3 |
| Golia, C. |
AEROTHERMODYNAMIC FIELD PAST
A REENTRY CAPSULE FOR SAMPLE RETURN MISSIONS |
ICAS2012-3.8.1 |
| Gollnick, V. |
A KNOWLEDGE BASED APPROACH
FOR EXTENDED PHYSICS-BASED WING MASS ESTIMATION IN EARLY DESIGN STAGES |
ICAS2012-1.1.1 |
| Gollnick, V. |
THE EREA VISION ON HIGH
PRIORITY RESEARCH AXES TOWARDS AIR TRANSPORT SYSTEM 2050 |
ICAS2012-1.7.1 |
| Gollnick, V. |
COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS2012-1.9.1 |
| Gollnick, V. |
SYSTEM ANALYSIS OF
PROGNOSTICS AND HEALTH MANAGEMENT SYSTEMS FOR FUTURE TRANSPORT AIRCRAFT |
ICAS2012-12.3.1 |
| Gollnick, V. |
MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS2012-6.4.1 |
| Golzad, I. |
FINDING TUNING FREQUENCY OF
SYMMETRIC AND ANTI-SYMMETRIC LAMB WAVES USING FEM |
ICAS2012-P3.6 |
| Goman, M. |
AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS2012-3.1.2 |
| Goman, M. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
| Gong, C. |
DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS2012-10.4.1 |
| Gonzalez, F. |
HYBRID GAME EVOLUTIONARY
ALGORITHM FOR MISSION PATH PLANNING OF AERIAL SURVEY TASKS |
ICAS2012-11.7.3 |
| Gonzalez, F. |
A CAPABILITY FRAMEWORK FOR
MULTIPLE HETEROGENEOUS UAVS: FROM A MISSION COMMANDER'S PERSPECTIVE |
ICAS2012-9.7.3 |
| Gonzalez, L. F. |
ROBUST AERODYNAMIC DESIGN
OPTIMISATION OF MORPHING AEROFOIL/WING USING DISTRIBUTED MOGA |
ICAS2012-11.10.3 |
| Gonzalez, L. F. |
DESIGN, SIMULATION AND
ANALYSIS OF A PARALLEL HYBRID-ELECTRIC PROPULSION SYSTEM FOR UNMANNED AERIAL
VEHICLES |
ICAS2012-4.5.1 |
| Gonzalez, L. F. |
MULTIDISCIPLINARY DESIGN AND
FLIGHT TESTING OF A REMOTE GAS/PARTICLE AIRBORNE SENSOR SYSTEM |
ICAS2012-6.10.4 |
| Gooden, J. H. M. |
THE EFFECT OF CROSSWIND ON
ENGINE INGESTION DURING TAKEOFFS FROM WATER CONTAMINATED RUNWAYS |
ICAS2012-9.1.2 |
| Gooding, C. L. |
PILOT CONVECTIVE WEATHER
DECISION MAKING IN EN ROUTE AIRSPACE |
ICAS2012-10.4.3 |
| Goodwin, A. |
AGEING AIRCRAFT SYSTEMS
& COST EFFECTIVE SAFETY |
ICAS2012-12.3.2 |
| Gopal, M. |
PRODUCTION
OF BIO-FUEL FROM ALGAE BIOMASS, NANNOCHLOROPSIS OCULATA, FOR ADDITION TO
KEROSENE JET A-1 |
ICAS2012-8.6.4 |
| Goraj, Z. |
DESIGN AND CONFIGURATION
LAYOUTS OF AN ADVANCED LONG ENDURANCE UAV- LESSONS LEARNT AFTER FLIGHT
TESTING |
ICAS2012-1.11.3 |
| Gorbushin, A. R. |
AN EXPERIENCE OF USING
NUMERICAL METHODS IN EXPERIMENTAL INVESTIGATIONS OF TsAGI |
ICAS2012-P2.6 |
| Gores, I. |
EVALUATION OF CABIN
DISPLACEMENT VENTILATION UNDER FLIGHT CONDITIONS |
ICAS2012-6.10.2 |
| Gosse, J. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
| Gostelow, J. P. |
STREAMWISE AND CROSSFLOW
INSTABILITIES ON INCLINED CIRCULAR CYLINDERS |
ICAS2012-3.10.2 |
| Gotseluk, T. B. |
COMPUTATIONAL AND
EXPERIMENTAL RESEARCH OF BOLT JOINTS OF METAL AND COMPOSITE IN AIRFRAMES |
ICAS2012-8.4.ST |
| Gowree, E. R. |
RECENT DEVELOPMENTS TO THE
VISCOUS GARABEDIAN AND KORN METHOD |
ICAS2012-2.11.3 |
| Gowree, E. R. |
A COMPUTATIONAL STUDY OF THE
AERODYNAMICS OF A SPINNING CYLINDER IN CROSSFLOW OF HIGH REYNOLDS NUMBER |
ICAS2012-3.11.2 |
| Grawunder, M. |
FLOW CHARACTERISTICS OF A
HELICOPTER FUSELAGE CONFIGURATION INCLUDING A ROTATING ROTOR HEAD |
ICAS2012-2.7.3 |
| Greco, P. C. |
THE INFLUENCE OF DEMOISELLE
AIRCRAFT ON LIGHT AND GENERAL AVIATION DESIGN |
ICAS2012-1.7.ST |
| Greco, P. C. |
TRAILING EDGE TREATMENT TO
ENHANCE HIGH LIFT SYSTEM PERFORMANCE |
ICAS2012-3.2.3 |
| Grendysa, W. |
DESIGN AND CONFIGURATION
LAYOUTS OF AN ADVANCED LONG ENDURANCE UAV- LESSONS LEARNT AFTER FLIGHT
TESTING |
ICAS2012-1.11.3 |
| Grigoryev, M. A. |
FLIGHT TESTS OF TRANSPORT
AIRCRAFT UPSET RECOVERY TECHNIQUES AND THE SYSTEM OF INFORMATION SUPPORT OF
CREW |
ICAS2012-5.1.1 |
| Grilli, A. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
| Grinev, K. N. |
EFFECTS OF MANIPULATOR TYPE
AND FEEL SYSTEM CHARACTERISTICS ON HIGH-FREQUENCY BIODYNAMIC PILOT-AIRCRAFT
INTERACTION |
ICAS2012-5.9.3 |
| Groen, E. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
| Grondel, S. |
AEROELASTIC SIMULATION OF
FLEXIBLE FLAPPING WING BASED ON STRUCTURAL FEM AND QUASI-STEADY AERODYNAMIC
MODEL |
ICAS2012-8.5.1 |
| Grunewald, E. |
DELPHI SURVEY 'LEVEL OF
SERVICE FOR AVIATION INFRASTRUCTURE MARKETS?' |
ICAS2012-10.2.3 |
| Gubanov, A. A. |
NUMERICAL RESEARCH OF THE
AIR INTAKE LOCATION INFLUENCE ONTO THE HIGH-SPEED AIRCRAFT PERFORMANCE |
ICAS2012-P2.1 |
| Guerrero, M. J. |
LEGAL AND TECHNICAL
IMPLICATIONS OF THE SAFETY RECOMMENDATIONS ISSUED IN THE FINAL REPORTS OF THE
CIVIL AIR ACCIDENTS AND INCIDENTS INVESTIGATIONS |
ICAS2012-9.4.ST |
| Guglieri, G. |
AN INNOVATIVE MISSION
MANAGEMENT SYSTEM FOR FIXED-WING UAVS |
ICAS2012-11.7.1 |
| Guillaume, M. |
SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS2012-10.6.1 |
| Gulbis, A. A. |
MODELING OF FLUID CONDITION
OF AIRCRAFT HYDRAULIC SYSTEM |
ICAS2012-6.6.2 |
| Gunnion, A. J. |
CRITICAL ASSESSMENT OF
FAILURE CRITERION FOR ADHESIVELY BONDED COMPOSITE JOINT REPAIR DESIGN |
ICAS2012-12.2.2 |
| Guo, R. |
A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
| Guo, W. G. |
THE DYNAMIC BEHAVIOR OF
FUNCTIONALLY GRADED PLATES UNDER THE IMPACT LOADING |
ICAS2012-7.7.3 |
| Gurak, D. |
METHODS FOR EVALUATION OF
AIRCRAFT MASS DISTRIBUTION |
ICAS2012-1.1.3 |
| Gurak, D. |
TOOL DEVELOPMENT FOR
AIRCRAFT LOADS POST-PROCESSING |
ICAS2012-P3.5 |
| Gustafsson, P. |
EXTERNAL AERODYNAMIC
PRESSURE LOADS FOR A RIGID FIGHTER AIRCRAFT, A COMPARISON BETWEEN PSP AND CFD |
ICAS2012-10.6.2 |
| Gutierrez, L. B. |
UAS DESIGN REQUIREMENTS FOR
OPERATION IN COLOMBIAN MOUNTAIN ENVIRONMENTS |
ICAS2012-1.8.ST |
| Hadda, J. El |
NOVEL PASSIVE AND ACTIVE
FLOW CONTROL FOR HIGH LIFT |
ICAS2012-3.7.2 |
| Hahn, M. |
BOUNDARY LAYER TRANSITION
DETECTION USING TEMPERATURE SENSITIVE PAINT IN THE ARA TRANSONIC WIND TUNNEL |
ICAS2012-3.4.2 |
| Haikola, T. |
DIARC PLASMA COATING FOR
RELIABLE AND DURABLE STRUCTURAL BONDING OF METALS |
ICAS2012-7.2.1 |
| Halfmann, N. |
THE DEVELOPMENT OF PRODUCT
AND ASSEMBLY CONCEPTS FOR AIRCRAFT CABIN INTEGRATION |
ICAS2012-9.9.1 |
| Hamid, M. F. A. |
COMPUTATIONAL STUDY ON THE
INFLUENCE OF COANDA JET ON AIRFOILS: TWO-DIMENSIONAL CASE |
ICAS2012-4.6.ST2 |
| Hamidiyanfar, A. |
AN
OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES |
ICAS2012-6.5.ST |
| Han, B. |
FINITE ELEMENT SIMULATION OF
CRACK PROPAGATION IN MILITARY AIRCRAFT COATINGS |
ICAS2012-7.2.3 |
| Han, Z. H. |
COMPARISON OF INFILL
SAMPLING CRITERIA IN KRIGING-BASED AERODYNAMIC OPTIMIZATION |
ICAS2012-11.10.ST |
| Han, Z. -H. |
MULTIDISCIPLINARY EVALUATION
OF TRUSS-BRACED WING FOR FUTURE GREEN AIRCRAFT |
ICAS2012-1.10.ST |
| Han, Z. -H. |
DESIGN OF LAMINAR
SUPERCRITICAL AIRFOILS BASED ON NAVIER-STOKES EQUATIONS |
ICAS2012-2.2.2 |
| Hantrais-Gervois, J. -L. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
| Hara, T. |
MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1.ST2 |
| Harada, A. |
FLIGHT TRAJECTORY
OPTIMIZATION FOR AN EFFICIENT AIR TRANSPORTATION SYSTEM |
ICAS2012-5.8.3 |
| Haraguchi, S. |
ANALYTICAL INVESTIGATIONS ON
LIGHT-WEIGHT STRUCTURES FOR SATELLITE STRUCTURAL FRAME APPLICATIONS THROUGH
3D MODELING |
ICAS2012-7.8.3 |
| Haraldsdottir, A. |
THE GENERALIZED ARRIVAL
PLANNER (GARP): MODELING AND ANALYSIS FOR ARRIVAL PLANNING |
ICAS2012-10.9.3 |
| Harel, M. |
A PERSONAL PLANE AIR
TRANSPORTATION SYSTEM: THE PPLANE PROJECT |
ICAS2012-10.5.1 |
| Harin, E. G. |
METHODS AND FACILITIES TO BE
USED TO EVALUATE THE AIRCRAFT FLIGHT AND NAVIGATION EQUIPMENT IN FLIGHT TESTS |
ICAS2012-5.6.3 |
| Harribey, T. |
MODELING OF THE INTERACTION
BETWEEN A TURBULENT FLOW AND AN ABLATABLE MATERIAL |
ICAS2012-3.8.2 |
| Harris, J. |
ON THE EFFECT OF DISTRIBUTED
ROUGHNESS ON TRANSITION OVER ROTOR-STATOR DEVICES |
ICAS2012-3.10.4 |
| Harrison, T. J. |
INITIAL RESULTS FROM DSTO’S
CORROSION STRUCTURAL INTEGRITY ROADMAP |
ICAS2012-12.6.1 |
| Harrison, T. J. |
INTERGRANULAR CORROSION
PROTOCOL DEVELOPMENT FOR 7075-T651 EXTRUSION |
ICAS2012-P3.3 |
| Hartley, D. L. |
DEVELOPMENT OF AN INTEGRATED
INFORMATION MANAGEMENT SYSTEM FOR AIRCRAFT STRUCTURAL TEST PROGRAMS |
ICAS2012-9.2.1 |
| Harvey, J. |
FLEXIBILITY OF AN ORITHOPTER
WING TESTED IN A WIND-TUNNEL |
ICAS2012-12.5.3 |
| Harvey, J. R. |
HARDWARE-IN-THE-LOOP
SIMULATION OF FUEL-CELL-BASED HYBRID-ELECTRICAL UAV PROPULSION |
ICAS2012-4.5.2 |
| Harvey, J. R. |
DEVELOPMENT OF A
HYBRID-ELECTRIC POWER-SYSTEM MODEL FOR A SMALL SURVEILLANCE AIRCRAFT |
ICAS2012-P6.4 |
| Haselbach, F. |
HOT END TECHNOLOGY FOR
ADVANCED, LOW EMISSION LARGE CIVIL AIRCRAFT ENGINES |
ICAS2012-4.10.2 |
| Hashimoto, A. |
NUMERICAL STUDY OF THE
EFFECTS OF CROSS-WIND ON THE JET BLAST DEFORMATION |
ICAS2012-10.10.3 |
| Hashimoto, A. |
AUTOMATIC HANDLING OF
DEFECTIVE SURFACE GEOMETRY WITHIN GRID GENERATION FOR NAVIER-STOKES
COMPUTATION |
ICAS2012-2.11.1 |
| Hashimoto, A. |
DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11.ST |
| Hassan, S. |
EFFECT ON THE AERODYNAMIC
FORCING IN AN AXIAL TURBINE STAGE ON VARYING STATOR BLADE SHAPE |
ICAS2012-4.3.ST |
| Hatanaka, K. |
A FULLY AUTOMATED CAD-BASED
FRAMEWORK FOR SHAPE OPTIMIZATION |
ICAS2012-11.10.1 |
| Hatano, T. |
CONTINUOUS DESCENT
TRAJECTORY WITH OPTIMUM ARRIVAL TIME CONTROLLABILITY |
ICAS2012-P8.3 |
| Hattori, S. |
EXPERIMENTAL STUDY OF
SUPERSONIC INLET FOR SUPPRESSION OF BUZZ IN SUBCRITICAL OPERATION |
ICAS2012-6.2.1 |
| Haucke, F. |
ACTIVE
SEPARATION CONTROL ON A 2D HIGH-LIFT WING SECTION TOWARDS HIGH REYNOLDS
NUMBER APPLICATION |
ICAS2012-3.5.3 |
| Hawkins, S. C. |
AN INVESTIGATION OF MODE I
FRACTURE TOUGHNESS USING ALIGNED CARBON-NANOTUBE FORESTS AT THE CRACK
INTERFACE |
ICAS2012-7.3.2 |
| Hazbon, O. |
UAS DESIGN REQUIREMENTS FOR
OPERATION IN COLOMBIAN MOUNTAIN ENVIRONMENTS |
ICAS2012-1.8.ST |
| He, J. |
ANALYTICAL INVESTIGATIONS ON
LIGHT-WEIGHT STRUCTURES FOR SATELLITE STRUCTURAL FRAME APPLICATIONS THROUGH
3D MODELING |
ICAS2012-7.8.3 |
| He, Y. H. |
ENGINEERING FAILURE MODES
AND FRACTURE CHARACTERISTICS OF SINGLE CRYSTAL SUPERALLOY BLADES |
ICAS2012-4.2.ST |
| He, Y. T. |
RESEARCH ON CRACK GROWTH OF
MULTIPLE-SITE DAMAGED STRUCTURE |
ICAS2012-7.1.3 |
| Hecker, P. |
DYNAMIC SEPARATION MINIMA
COUPLED WITH WAKE VORTEX PREDICTIONS IN DEPENDENT RUNWAY CONFIGURATIONS |
ICAS2012-10.4.2 |
| Hecker, P. |
GBAS CURVED APPROACH
PROCEDURES: ADVANTAGES, CHALLENGES AND APPLICABILITY |
ICAS2012-4.9.2 |
| Heib, S. |
THE ONERA ELSA CFD SOFTWARE
: INPUT FROM RESEARCH AND FEEDBACK FROM INDUSTRY |
ICAS2012-2.1.1 |
| Heider, A. |
EVALUATION OF CABIN
DISPLACEMENT VENTILATION UNDER FLIGHT CONDITIONS |
ICAS2012-6.10.2 |
| Heitzmann, M. |
INTERFACE DIFFUSION AND
MORPHOLOGY OF AEROSPACE GRADE EPOXY CO-CURED WITH THERMOPLASTIC POLYMERS |
ICAS2012-7.8.2 |
| Helldin, T. |
AUTOMATION GUIDELINES FOR
INTRODUCING SURVIVABILITY ANALYSIS IN FUTURE FIGHTER AIRCRAFT |
ICAS2012-9.1.1 |
| Heltsch, N. |
ASSESSMENT OF STRUCTURAL
EFFECT OF SELECTIVE STITCHING ON COMPOSITE SKIN-STIFFENER BONDING |
ICAS2012-8.9.1 |
| Hendrick, P. |
DESIGN AND AERO-ELASTIC
OPTIMISATION OF THE STRUCTURE OF THE LAPCAT A2 MACH 5 AIRLINER |
ICAS2012-8.4.3 |
| Henner, M. |
TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS2012-4.4.4 |
| Hermetz, J. |
EOLE, AN INNOVATIVE FLYING
SCALE DEMONSTRATOR FOR AIR-LAUNCH-TO-ORBIT AUTOMATIC SYSTEMS |
ICAS2012-1.11.2 |
| Hernando, J. -L. |
CARRIER SUITABILITY OF
LAND-BASED AIRCRAFT |
ICAS2012-1.1.ST |
| Higashino, K. |
DEVELOPMENT OF A SMALL-SCALE
SUPERSONIC FLIGHT EXPERIMENT VEHICLE AS A FLYING TEST BED |
ICAS2012-1.2.2 |
| Higashiyama, Y. |
DEVELOPMENT OF LAPTOP PC
TOOL WITH VISUAL PROJECTION FOR FLIGHT MANAGEMENT TRAINING |
ICAS2012-9.10.ST |
| Higuchi, T. |
COLLISION AVOIDANCE OF
INDOOR FLYING DOUBLE TETRAHEDRON HEXA-ROTORCRAFT |
ICAS2012-11.5.1 |
| Hinckley, S. |
DISTRIBUTED
OPTICAL FIBRE SMART SENSORS FOR ADVANCE SENSING SYSTEMS IN AEROSPACE VEHICLES |
ICAS2012-P6.7 |
| Hino, T. |
REAL TIME PATH PLANNING
METHOD OF AIRCRAFT FORMATIONS |
ICAS2012-11.7.2 |
| Hiraoka, K. |
COMPARISON OF PERFORMANCE OF
PROPELLER BLADES BY DIFFERENCE IN PLANAR SHAPE |
ICAS2012-4.6.ST1 |
| Hishida, M. |
DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11.ST |
| Ho, D. |
INVESTIGATION OF LOW THRUST
TO WEIGHT RATIO ROTATIONAL CAPACITY OF ASYMMETRIC MONO-WING CONFIGURATIONS |
ICAS2012-1.4.3 |
| Hoeijmakers, H. W. M. |
NUMERICAL METHOD FOR ICE
ACCRETION ON 3D WINGS |
ICAS2012-2.6.1 |
| Hoeijmakers, H. W. M. |
EXPERIMENTAL/NUMERICAL
INVESTIGATION AIRFOIL WITH FLOW CONTROL BY SYNTHETIC JETS |
ICAS2012-3.7.5 |
| Hoffler, K. |
CONCEPT OF INTEGRATION FOR
UAS OPERATIONS IN THE NAS |
ICAS2012-10.7.1 |
| Holsten, J. |
MODEL VALIDATION OF A
TILTWING UAV IN TRANSITION PHASE APPLYING WINDTUNNEL INVESTIGATIONS |
ICAS2012-11.1.1 |
| Holsten, J. |
CONTROL CONCEPT OF A
TILTWING UAV DURING LOW SPEED MANOEUVRING |
ICAS2012-11.1.2 |
| Hölzel, N. B. |
SYSTEM ANALYSIS OF
PROGNOSTICS AND HEALTH MANAGEMENT SYSTEMS FOR FUTURE TRANSPORT AIRCRAFT |
ICAS2012-12.3.1 |
| Honda, M. |
D-SEND PROJECT FOR LOW SONIC
BOOM DESIGN TECHNOLOGY |
ICAS2012-1.2.1 |
| Honnery, D. |
DEVELOPMENT OF A
HYBRID-ELECTRIC POWER-SYSTEM MODEL FOR A SMALL SURVEILLANCE AIRCRAFT |
ICAS2012-P6.4 |
| Hordé, T. |
APACHE : INTEGRATED HYBRID
FUEL CELL SYSTEM FOR 2-SEAT ALL ELECTRIC AIRCRAFTS PROPULSION |
ICAS2012-6.7.4 |
| Hornung, M. |
MULTI-DISCIPLINARY DESIGN
AND FEASIBILITY STUDY OF DISTRIBUTED PROPULSION SYSTEMS |
ICAS2012-1.7.5 |
| Hornung, M. |
AIRPORT CAPACITY
REPRESENTATION BASED ON AIRSIDE SIMULATIONS |
ICAS2012-10.10.1 |
| Hornung, M. |
A SCENARIO-BASED APPROACH TO
DEVELOP REPRESENTATIVE TRAFFIC ENVIRONMENTS FOR OPERATIONAL AIRCRAFT
EVALUATION |
ICAS2012-6.3.1 |
| Hospers, J. M. |
NUMERICAL METHOD FOR ICE
ACCRETION ON 3D WINGS |
ICAS2012-2.6.1 |
| Hospodar, P. |
GLOBAL OPTIMIZATION OF
TWO-DIMENSIONAL HIGH LIFT AERODYNAMIC SYSTEM |
ICAS2012-11.10.2 |
| Hospodar, P. |
STABILIZATION OF
LONGITUDINAL AIRCRAFT MOTION USING MODEL PREDICTIVE CONTROL AND EXACT
LINEARIZATION |
ICAS2012-P5.11 |
| Hosseini Kordkheili, S. A. |
APPLICATION
OF SINGULAR VALUE DECOMPOSITION IN COMPONENT MODE SYNTHESIS WITH EXPERIMENTAL
APPROACH |
ICAS2012-8.11.3 |
| Hosseini, A. |
AN
APPROXIMATE ENGINEERING METHOD FOR AERODYNAMIC HEATING SOLUTION AROUND BLUNT
BODY NOES |
ICAS2012-11.4.4 |
| Hou, J. |
PRE-STRESSED MODAL ANALYSIS
OF A TURBINE SPACER |
ICAS2012-P4.11 |
| Hou, M. |
INTERFACE DIFFUSION AND
MORPHOLOGY OF AEROSPACE GRADE EPOXY CO-CURED WITH THERMOPLASTIC POLYMERS |
ICAS2012-7.8.2 |
| Hou, T. |
EXPERIMENTAL DEVELOPMENT AND
ANALYSIS OF AN ACTIVE CRUSHING ELEMENT USING PRESSURIZED COMPOSITE TUBES |
ICAS2012-8.1.ST |
| Howarth, D. |
OPTIMIZING DESIGN
SPECIFICATIONS FROM AIRCRAFT MARKET ECONOMICS |
ICAS2012-6.3.4 |
| Hsu, H. -T. |
THE AFFECT OF SCREEN SIZE ON
MISSION COMMANDER’S SITUATION AWARENESS |
ICAS2012-9.7.5 |
| Hu, Y. |
AERODYNAMICS ANALYSIS OF
CYCLOIDAL ROTOR |
ICAS2012-2.7.1 |
| Huang, J. B. |
INVESTIGATION OF PASSIVE
FLOW CONTROL METHODOLOGIES USING SST-IDDES |
ICAS2012-P2.7 |
| Huang, J. -T. |
NUMERICAL SIMULATION OF
TRANSONIC SHOCK-VORTEX INTERACTION FLOW AROUND THE VFE-2 DELTA WING BASED ON
MDDES |
ICAS2012-P2.4 |
| Huang, L. |
WING-BODY OPTIMIZATION BASED
ON MULTI-FIDELITY SURROGATE MODEL |
ICAS2012-11.10.5 |
| Huang, W. |
RESEARCH FOR JET FLOW INFLUENCES TO WING-MOUNTED CIVIL
AIRCRAFT AERODYNAMIC CHARACTERISTICS |
ICAS2012-2.9.1 |
| Huang, X. |
CRACK NUCLEATION MODELING IN
NOTCHED SPECIMEN SUBJECTED TO HIGH FATIGUE LOADING |
ICAS2012-7.7.4 |
| Huby, G. M. |
DEVELOPING THE USE OF
NEURAL-NETWORK TEST TECHNOLOGY FROM AVIONICS TO WIRING SYSTEMS |
ICAS2012-12.5.1 |
| Hue, D. |
AUTOMATED CHAIN FOR
AERODYNAMIC COMPUTATIONS MEETING AIRCRAFT TRIMMING REQUIREMENTS |
ICAS2012-2.10.1 |
| Hühne, C. |
SEMI-ANALYTICAL SPRING-IN
ANALYSIS TO COUNTERACT CFRP MANUFACTURING DEFORMATIONS BY TOOL COMPENSATION |
ICAS2012-8.2.2 |
| Hui, K. |
INNOVATIVE
MOISTURE/ICING-RESISTANT FLUSH AIR DATA SYSTEM |
ICAS2012-6.5.1 |
| Hung, J. Y. -C. |
DESIGN, SIMULATION AND
ANALYSIS OF A PARALLEL HYBRID-ELECTRIC PROPULSION SYSTEM FOR UNMANNED AERIAL
VEHICLES |
ICAS2012-4.5.1 |
| Hwang, Y. H. |
TERRAIN REFERENCED UAV
NAVIGATION WITH LIDAR - A COMPARISON OF SEQUENTIAL PROCESSING AND BATCH
PROCESSING ALGORITHMS |
ICAS2012-P5.7 |
| Idris, A. |
PERFORMANCE TEST OF A
SMALL-SCALE TURBOJET ENGINE RUNNING ON A PALM OIL BIODIESEL - JET A BLEND |
ICAS2012-4.8.1 |
| Idris, A. C. |
EXPERIMENTAL STUDIES ON
MICRO-VORTEX GENERATORS IN HYPERSONIC FLOW |
ICAS2012-3.5.2 |
| Inada, Y. |
AERODYNAMIC CHARACTERISTICS
OF A BIRD-LIKE ASSEMBLED WING |
ICAS2012-P2.22 |
| Inada, Y. |
FORMATION SHAPE CONTROL OF
UNMANNED AIR VEHICLES |
ICAS2012-P5.8 |
| Inada, Y. |
GUST RESPONSE ANALYSIS IN
THE FLIGHT FORMATION OF UNMANNED AIR VEHICLES |
ICAS2012-P5.9 |
| Inagawa, N. |
DEVELOPMENT OF OBSERVATIONAL
SYSTEM WITH UNMANNED FLIGHT SYSTEM |
ICAS2012-P5.10 |
| Inoue, Y. |
DEVELOPMENT OF SUPERSONIC
NATURAL LAMINAR FLOW WING DESIGN SYSTEM USING CFD-BASED INVERSE METHOD |
ICAS2012-2.2.1 |
| Ireland, M. |
DEVELOPMENT OF NAVIGATION
ALGORITHMS FOR NAP-OF-THE-EARTH UAV FLIGHT IN A CONSTRAINED URBAN ENVIRONMENT |
ICAS2012-11.9.1 |
| Isa, M. D. |
DAMAGE TOLERANCE OF Z-PINNED
COMPOSITE JOINTS |
ICAS2012-7.5.2 |
| Ishida, T. |
AUTOMATIC HANDLING OF
DEFECTIVE SURFACE GEOMETRY WITHIN GRID GENERATION FOR NAVIER-STOKES
COMPUTATION |
ICAS2012-2.11.1 |
| Ishikawa, H. |
DEVELOPMENT OF SUPERSONIC
NATURAL LAMINAR FLOW WING DESIGN SYSTEM USING CFD-BASED INVERSE METHOD |
ICAS2012-2.2.1 |
| Ishikawa, T. |
LESSONS LEARNED IN FULL
COMPOSITE AERO-STRUCTURES DEVELOPMENT IN JAPAN |
ICAS2012-0.3 |
| Ishiko, K. |
NUMERICAL STUDY OF THE
EFFECTS OF CROSS-WIND ON THE JET BLAST DEFORMATION |
ICAS2012-10.10.3 |
| Ishiko, K. |
DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11.ST |
| Ishmuratov, F. |
ANALYSIS OF STATIC AND
DYNAMIC AEROELASTIC CHARACTERISTICS OF AIRPLANE IN TRANSONIC FLOW |
ICAS2012-8.10.4 |
| Ishmuratov, F. |
AEROELASTIC
MULTIDISCIPLINARY ANALYSIS OF THE FIN
WITH INNOVATIVE ADAPTIVE CONTROL |
ICAS2012-8.7.4 |
| Isikdogan, O. |
METHODS FOR EVALUATION OF
AIRCRAFT MASS DISTRIBUTION |
ICAS2012-1.1.3 |
| Isikveren, A. T. |
MULTI-DISCIPLINARY DESIGN
AND FEASIBILITY STUDY OF DISTRIBUTED PROPULSION SYSTEMS |
ICAS2012-1.7.5 |
| Isikveren, A. T. |
PROGRESS AND PERSPECTIVES OF
ELECTRIC AIR TRANSPORT |
ICAS2012-8.6.1 |
| Isogai, K. |
NUMERICAL SIMULATION OF
SHOCK-STALL FLUTTER OF A HIGH-ASPECT-RATIO FORWARD-SWEPT WING |
ICAS2012-8.10.2 |
| Isogai, K. |
INVESTIGATION ON STRUCTURAL
AND AERODYNAMIC CHARACTERISTICS OF RESONANT TYPE ELASTIC FLAPPING WING |
ICAS2012-9.5.3 |
| Isozumi, R. |
THEORETICAL AND EXPERIMENTAL
INVESTIGATIONS ON CHOKING PHENOMENA OF AXISYMMETRIC CONVERGENT NOZZLE FLOW |
ICAS2012-P2.11 |
| Itabashi, N. |
FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS2012-5.2.1 |
| Itano, K. |
DEVELOPMENT AND EVALUATION
OF FATIGUE AND DROWSINESS PREDICTOR |
ICAS2012-9.6.1 |
| Ito, T. |
EXPERIMENTAL STUDY OF THE
MORPHING FLAP AS A LOW NOISE HIGH LIFT DEVICE FOR AIRCRAFT WING |
ICAS2012-9.11.3 |
| Ito, T. |
EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS2012-9.3.1 |
| Itoh, E. |
ANALYZING SEPARATION LOSS
EVENTS IN TWO-PAIRED AIRCRAFT TRAILING CONDUCTING AIRBORNE TIME SPACING BASED
CONTINUOUS DESCENT ARRIVAL |
ICAS2012-10.8.3 |
| Iuspa, L. |
DESIGN OF MASS SAVING
CONFIGURATIONS FOR WINGED REENTRY VEHICLES |
ICAS2012-1.5.3 |
| Ivanov, D. |
NUMERICAL SIMULATION OF
THREE-DIMENSIONAL SHOCK-WAVE/BOUNDARY-LAYER INTERACTION ON SHARP AND BLUNTED
FLAT PLATE |
ICAS2012-2.4.2 |
| Ivanov, M. J. |
INTERDISCIPLINARY COMPLEX
DESIGN OF MODERN HIGH AND LOW PRESSURE TURBINES |
ICAS2012-4.3.3 |
| Iwahori, Y. |
EVALUATION ON DISCRETE
SOURCE DAMAGES OF CFRP STIFFENED PANELS |
ICAS2012-7.7.1 |
| Jahanmiri, M. |
MEASUREMENTS AND PREDICTION
OF LAMINAR-TURBULENT TRANSITION AT HIGH FREE-STREAM TURBULENCE & PRESSURE
GRADIENTS |
ICAS2012-3.10.5 |
| Janardhana, M. |
EFFECT OF OFF-NORMAL LOADING
ON THE BOND STRENGTH MEASUREMENT OF BONDED REPAIRS |
ICAS2012-12.2.1 |
| Janardhana, M. |
MICROSTRUCTURE AND
MECHANICAL PROPERTIES OF LASER CLADDING REPAIR OF AISI 4340 STEEL |
ICAS2012-12.4.4 |
| Janik, W. |
A COMPOSITE AND
METAL JOINT FOR A PROPELLER BLADE ROOT |
ICAS2012-7.5.3 |
| Jansen, D. |
NOVEL PASSIVE AND ACTIVE
FLOW CONTROL FOR HIGH LIFT |
ICAS2012-3.7.2 |
| Jarvis, R. A. |
DEVELOPMENT OF A
HYBRID-ELECTRIC POWER-SYSTEM MODEL FOR A SMALL SURVEILLANCE AIRCRAFT |
ICAS2012-P6.4 |
| Jebens, K. |
ARTIFICIAL HINGED-WING
BIRD WITH ACTIVE TORSION AND PARTIALLY
LINEAR KINEMATICS |
ICAS2012-3.6.1 |
| Jemitola, P. O. |
BOX WING AIRCRAFT CONCEPTUAL
DESIGN |
ICAS2012-1.9.ST |
| Jeong, M. -S. |
AEROELASTIC ANALYSIS FOR
HELICOPTER ROTOR BLADES IN HOVER AND FORWARD FLIGHTS |
ICAS2012-11.5.3 |
| Jeung, I. -S. |
EFFECT OF VENT MIXER TO
MIXING CHARACTERISTICS IN SUPERSONIC FLOW |
ICAS2012-P4.4 |
| Ji, P. -B. |
MULTIDISCIPLINARY EVALUATION
OF TRUSS-BRACED WING FOR FUTURE GREEN AIRCRAFT |
ICAS2012-1.10.ST |
| Jia, H. |
A CASE STUDY OF ARRIVAL AND
DEPARTURE MANAGERS COOPERATION FOR REDUCING AIRBORNE HOLDING TIMES AT
DESTINATION AIRPORTS |
ICAS2012-10.1.ST |
| Jia, M. |
ANALYZING AND MODELING OF
JAMMING DESTROY FACTOR |
ICAS2012-P6.1 |
| Jia, Y. -Y. |
NUMERICAL STUDY ON RESIDUAL
THERMAL STRESSES IN CARBON FIBRE PULLOUT |
ICAS2012-7.3.1 |
| Jiang, X. |
MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1.ST2 |
| Jimin, K. |
AN INTEGRATED FRAMEWORK FOR
INNOVATIVE COMPOUND GYROPLANE DESIGN SYSTEM |
ICAS2012-1.4.ST |
| Jo, M. -S. |
VERIFICATION OF OPTICAL
PAYLOAD CFRP STRUCTURE FOR SATELLITE THROUGH ANALYSIS AND SPACE QUALIFICATION
TEST |
ICAS2012-P3.9 |
| Johanning, A. |
NOVEL LOW-FLYING
PROPELLER-DRIVEN AIRCRAFT CONCEPT FOR REDUCED DIRECT OPERATING COSTS AND
EMISSIONS |
ICAS2012-1.10.5 |
| John, S. |
FLOW-INDUCED FLUTTER OF
SLENDER CANTILEVER HIGH-COMPLIANCE PLATES |
ICAS2012-8.10.5 |
| Johnson, W. W. |
PILOT CONVECTIVE WEATHER
DECISION MAKING IN EN ROUTE AIRSPACE |
ICAS2012-10.4.3 |
| Jon, A. |
A COMPUTATIONAL STUDY ON THE
DESIGN OF AIRFOILS FOR A FIXED WING MAV AND THE AERODYNAMIC CHARACTERISTIC OF
THE VEHICLE |
ICAS2012-2.2.ST |
| Jonas, M. |
DESIGN AND CONFIGURATION
LAYOUTS OF AN ADVANCED LONG ENDURANCE UAV- LESSONS LEARNT AFTER FLIGHT
TESTING |
ICAS2012-1.11.3 |
| Jones, D. P. |
COMPUTATIONAL AND
EXPERIMENTAL ANALYSIS OF THE ACTIVE MORPHING WING CONCEPT |
ICAS2012-2.5.3 |
| Jones, M. |
QUANTITATIVE FRACTOGRAPHY
MARKERS FOR DETERMINING FATIGUE CRACK GROWTH RATES IN ALUMINIUM AND TITANIUM
AIRCRAFT STRUCTURES |
ICAS2012-12.4.1 |
| Jones, M. B. |
FLEXIBILITY OF AN ORITHOPTER
WING TESTED IN A WIND-TUNNEL |
ICAS2012-12.5.3 |
| Jones, R. |
SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS2012-7.2.2 |
| Joo, S. |
OPTIMIZATION OF
TWO-DIMENSIONAL WING IN GROUND EFFECT CONSIDERING AERODYNAMIC CENTRE OF
HEIGHT AND LIFT |
ICAS2012-P2.15 |
| Joosten, M. W. |
IMPROVED DESIGN METHODS FOR
CRASHWORTHY COMPOSITE HELICOPTER STRUCTURES |
ICAS2012-8.1.2 |
| Jothiprasad, G. |
THE EFFECT OF PLASMA
ACTUATORS ON TIP CLEARANCE FLOWS IN COMPRESSOR ROTORS |
ICAS2012-4.4.1 |
| Jouannet, C. |
RECYCLING OLD WEIGHT
ASSESSMENT METHODS AND GIVING THEM NEW LIFE IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS2012-1.1.2 |
| Jouannet, C. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
| Joulia, A. |
AIRCRAFT 4D CONTRACT BASED
OPERATION: THE 4DCO-GC PROJECT |
ICAS2012-10.3.3 |
| Joyce, K. J. |
THE AUSTRALIAN ARMY AND
UNMANNED AERIAL VEHICLES… 2O YEARS AND FINALLY IN-SERVICE |
ICAS2012-1.11.1 |
| Jun, B. -E. |
AUTOPILOT DESIGN FOR AN
AGILE MISSILE USING L1 ADAPTIVE BACKSTEPPING CONTROL |
ICAS2012-P5.4 |
| Jung, S. |
COMPARATIVE EVALUATION OF
ICING ON AERODYNAMIC SURFACES |
ICAS2012-3.4.3 |
| Jupp, J. A. |
21ST CENTURY CHALLENGES FOR
THE DESIGN OF PASSENGER AIRCRAFT |
ICAS2012-1.10.1 |
| Juracka, J. |
THE DETERMINATION OF
DELAMINATION STRAIN ENERGY RELEASE RATE OF COMPOSITE BI-MATERIAL INTERFACE |
ICAS2012-7.4.1 |
| Justin, C. Y. |
A COMPETITIVE AND
REAL-OPTIONS FRAMEWORK FOR THE ECONOMIC ANALYSIS OF LARGE AEROSPACE PROGRAMS |
ICAS2012-6.3.2 |
| Kachel, S. |
A NEW APPROACH TO IDENTIFICATION AND OPTIMIZATION OF AIRFOILS
BY USING THE COMBINATORIAL-CYCLIC METHOD |
ICAS2012-P2.24 |
| Kaden, M. |
DESIGN, ANALYSIS AND
MANUFACTURING OF A THERMOPLASTIC UD CF-PEEK SLAT |
ICAS2012-6.1.1 |
| Kaden, M. |
REPAIR CONCEPT SUPPORTED BY
LASER REMOVAL AND INDUCTIVE HEATING |
ICAS2012-7.6.1 |
| Kafyeke, F. |
BOMBARDIER
C-SERIES AIRCRAFT DEVELOPMENT |
ICAS2012-0.5 |
| Kageyama, K. |
A BASIC STUDY ON EFFICIENCY IN JAPANESE
AIRSPACE |
ICAS2012-10.2.1 |
| Kajikawa, Y. |
SCIENCE AND TECHNOLOGY MAP
ANALYSIS OF AEROSPACE ENGINEERING |
ICAS2012-P7.1 |
| Kalinin, D. V. |
OPTIMAL HIGH-SPEED
HELICOPTER TRANSMISSION DESIGNS |
ICAS2012-P4.13 |
| Kameda, M. |
EXPERIMENTAL STUDY OF
SUPERSONIC INLET FOR SUPPRESSION OF BUZZ IN SUBCRITICAL OPERATION |
ICAS2012-6.2.1 |
| Kameda, M. |
PERFORMANCE EVALUATION OF A
BOUNDARY-LAYER DIVERTER FOR SUPERSONIC PROPULSION SYSTEM |
ICAS2012-6.2.2 |
| Kappel, E. |
SEMI-ANALYTICAL SPRING-IN
ANALYSIS TO COUNTERACT CFRP MANUFACTURING DEFORMATIONS BY TOOL COMPENSATION |
ICAS2012-8.2.2 |
| Kappenberger, C. |
HMIAC – SURVEY ON
HUMAN-MACHINE INTERACTION IN AIRCRAFT COCKPITS |
ICAS2012-9.7.4 |
| Kappenberger, C. |
A MODEL OF HORIZONTAL
TAILPLANE DAMAGE FOR USE IN FLIGHT DYNAMICS |
ICAS2012-P5.3 |
| Kaps, R. |
DESIGN, DEVELOPMENT AND
MANUFACTURING OF THE ALCAS CFRP DOOR SURROUND STRUCTURE |
ICAS2012-8.8.1 |
| Karas, O. V. |
AN EXPERIENCE IN AERODYNAMIC
DESIGN OF TRANSPORT AIRCRAFT |
ICAS2012-2.9.3 |
| Karas, O. V. |
ANALYSIS OF STATIC AND
DYNAMIC AEROELASTIC CHARACTERISTICS OF AIRPLANE IN TRANSONIC FLOW |
ICAS2012-8.10.4 |
| Katupitiya, J. |
DESIGN OF A mu SYNTHESIS
CONTROLLER TO STABILIZE AN UNMANNED HELICOPTER |
ICAS2012-11.5.2 |
| Katupitiya, J. |
A GREY-BOX SYSTEM
IDENTIFICATION PROCEDURE FOR SCALE MODEL HELICOPTERS BASED ON
FREQUENCY-DOMAIN ESTIMATION METHODS |
ICAS2012-11.9.ST |
| Kaushik, B. |
DESIGN METHODS FOR AN
UNCONVENTIONAL SPLIT WING AIRCRAFT CONFIGURATION |
ICAS2012-1.3.1 |
| Kawaguchi, J. |
GUIDANCE AND CONTROL LAW FOR
D-SEND#2 |
ICAS2012-5.3.1 |
| Kawamura, N. |
INSTABILITY CHARACTERISTICS
OF SHOCK WAVES AHEAD OF A HEMISPHERICAL SHELL AT SUPERSONIC SPEEDS |
ICAS2012-11.4.2 |
| Kawasaki, S. |
INTEGRATED DESIGN METHOD OF
A ROCKET ENGINE TURBOPUMP SUB-SYSTEM FOR SUPPRESSING ROTOR LATERAL VIBRATION |
ICAS2012-4.3.4 |
| Kawazoe, H. |
ANALYTIC METHOD FOR FLIGHT
MOTION OF AIRCRAFT WITH A SINGLE VIDEO CAMERA AND ITS APPLICATION TO A FREE
FLIGHT GLIDER |
ICAS2012-5.6.1 |
| Keane, A. J. |
MODELLING OF A WARPING WING
FOR ENERGY CONSUMPTION MINIMIZATION |
ICAS2012-1.3.4 |
| Keck, R. |
REPAIR CONCEPT SUPPORTED BY
LASER REMOVAL AND INDUCTIVE HEATING |
ICAS2012-7.6.1 |
| Keck, R. A. |
DESIGN, ANALYSIS AND
MANUFACTURING OF A THERMOPLASTIC UD CF-PEEK SLAT |
ICAS2012-6.1.1 |
| Kellner, S. |
AN ASSET FOR IMPROVED
EFFICIENCY AND PUNCTUALITY IN AIR TRANSPORT |
ICAS2012-11.7.5 |
| Kelly, D. |
A FEASIBILITY STUDY FOR
MULTI-MATERIAL RETROFITTABLE ENERGY ABSORBING STRUCTURE FOR AGED HELICOPTER
SUBFLOOR |
ICAS2012-12.3.3 |
| Kelly, D. |
DIRECTIONAL ENHANCEMENT OF
COMPOSITE STRUCTURES ENERGY ABSORPTION USING MAGNETORHEOLOGICAL FLUIDS |
ICAS2012-7.8.1 |
| Kelly, D. |
EXPERIMENTAL DEVELOPMENT AND
ANALYSIS OF AN ACTIVE CRUSHING ELEMENT USING PRESSURIZED COMPOSITE TUBES |
ICAS2012-8.1.ST |
| Kelly, D. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
| Kennedy, D. |
IMPROVED EXACT STRIP
POSTBUCKLING ANALYSIS FOR ANISOTROPIC PLATES WITH FIXED, FREE AND STRAIGHT
EDGES |
ICAS2012-8.2.1 |
| Kestek, H. |
TOOL DEVELOPMENT FOR
AIRCRAFT LOADS POST-PROCESSING |
ICAS2012-P3.5 |
| Khaletskiy, Y. |
STUDY ON NOISE OF COUNTER
ROTATING FAN MODELS AT CIAM ANECHOIC CHAMBER |
ICAS2012-3.9.4 |
| Kharkovsky, S. V. |
INTERDISCIPLINARY COMPLEX
DESIGN OF MODERN HIGH AND LOW PRESSURE TURBINES |
ICAS2012-4.3.3 |
| Khodagolian, V. |
AN EXPERIMENTAL STUDY OF A
PULSED AIR JET AND AN ACOUSTIC SYNTHETIC JET ON A LOW SPEED TURBULENT
BOUNDARY LAYER |
ICAS2012-3.5.1 |
| Khrabrov, A. |
AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS2012-3.1.2 |
| Khrabrov, A. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
| Kim, C. -H. |
EFFECT OF VENT MIXER TO
MIXING CHARACTERISTICS IN SUPERSONIC FLOW |
ICAS2012-P4.4 |
| Kim, D. -J. |
VERIFICATION OF OPTICAL
PAYLOAD CFRP STRUCTURE FOR SATELLITE THROUGH ANALYSIS AND SPACE QUALIFICATION
TEST |
ICAS2012-P3.9 |
| Kim, E. T. |
HIDDEN MARKOV MODEL
PARAMETER ESTIMATION FOR MULTIPLE DIM TARGET DETECTION |
ICAS2012-P6.5 |
| Kim, J. -H. |
A COMPUTATIONAL STUDY ON THE
DESIGN OF AIRFOILS FOR A FIXED WING MAV AND THE AERODYNAMIC CHARACTERISTIC OF
THE VEHICLE |
ICAS2012-2.2.ST |
| Kim, J. -H. |
UAV COLLISION AVOIDANCE VIA
OPTIMAL TRAJECTORY GENERATION METHOD |
ICAS2012-P5.5 |
| Kim, J. W. |
MODELING OF NO AND OH
INFRARED RADIATION ON A CONVERGENT-DIVERGENT NOZZLE |
ICAS2012-P4.6 |
| Kim, K. -H. |
A COMPUTATIONAL STUDY ON THE
DESIGN OF AIRFOILS FOR A FIXED WING MAV AND THE AERODYNAMIC CHARACTERISTIC OF
THE VEHICLE |
ICAS2012-2.2.ST |
| Kim, K. -S. |
A PEG-BASED ASCENDING
GUIDANCE ALGORITHM FOR RAMJET-POWERED VEHICLES |
ICAS2012-5.7.4 |
| Kim, S. |
AN INTEGRATED FRAMEWORK FOR
INNOVATIVE COMPOUND GYROPLANE DESIGN SYSTEM |
ICAS2012-1.4.ST |
| Kim, S. T. |
CFD COMPUTATION OF THE
GROUND EFFECT ON AIRPLANE WITH HIGH ASPECT RATIO WING |
ICAS2012-P2.23 |
| Kim, T. H. |
THERMAL ANALYSIS NEAR
SECONDARY INJECTION HOLE IN SITVC SYSTEM |
ICAS2012-P4.9 |
| Kim, Y. |
MULTIPLE UAV FORMATION
RECONFIGURATION WITH COLLISION AVOIDANCE GUIDANCE VIA DIFFERENTIAL GEOMETRY
CONCEPT |
ICAS2012-11.2.2 |
| Kim, Y. |
VISION-BASED UAV GUIDANCE
AND ESTIMATION FOR AERIAL TARGET TRACKING |
ICAS2012-11.3.2 |
| Kim, Y. |
CFD COMPUTATION OF THE
GROUND EFFECT ON AIRPLANE WITH HIGH ASPECT RATIO WING |
ICAS2012-P2.23 |
| Kim, Y. -H. |
TIME DEPENDENT ANALYSIS OF A
RECTANGULAR SYNTHETIC JET |
ICAS2012-3.7.1 |
| Kimmel, R. |
HIFIRE-1 BOUNDARY-LAYER
TRANSITION MEASUREMENTS |
ICAS2012-3.10.3 |
| Kindervater, C. |
IMPROVED DESIGN METHODS FOR
CRASHWORTHY COMPOSITE HELICOPTER STRUCTURES |
ICAS2012-8.1.2 |
| Kiper, T. |
METHODS FOR EVALUATION OF
AIRCRAFT MASS DISTRIBUTION |
ICAS2012-1.1.3 |
| Kistan, T. |
A PRACTICAL, ROUTE-BASED
APPROACH TO AIRSPACE CAPACITY MANAGEMENT |
ICAS2012-10.2.2 |
| Kleine, H. |
JET INTERACTION IN A
HYPERSONIC FLOW: A COMPARISON BETWEEN PLIF THERMOMETRY AND COMPUTATIONAL
SIMULATION |
ICAS2012-4.11.2 |
| Kleineberg, M. |
SENSOR AND
REAL-TIME-PROCESS-SIMULATION GUIDED AUTOCLAVE PROCESS CONTROL FOR COMPOSITE
PRODUCTION |
ICAS2012-6.1.2 |
| Kleineberg, M. |
DESIGN, DEVELOPMENT AND
MANUFACTURING OF THE ALCAS CFRP DOOR SURROUND STRUCTURE |
ICAS2012-8.8.1 |
| Klingauf, U. |
OPERATIONAL
HUMAN-IN-THE-LOOP INTEGRATION OF 4D ARRIVAL GUIDANCE |
ICAS2012-5.8.1 |
| Kmiecik, M. |
A HIGHLY EXPANDABLE LOW-COST
OPEN-SOURCE UAV SYSTEM WITH HIGH ON-BOARD PROCESSING POWER |
ICAS2012-1.8.1 |
| Kobayashi, R. |
DEVELOPMENT OF LAPTOP PC
TOOL WITH VISUAL PROJECTION FOR FLIGHT MANAGEMENT TRAINING |
ICAS2012-9.10.ST |
| Koh, T. M. |
DAMAGE TOLERANCE OF Z-PINNED
COMPOSITE JOINTS |
ICAS2012-7.5.2 |
| Kok, J. |
HYBRID GAME EVOLUTIONARY
ALGORITHM FOR MISSION PATH PLANNING OF AERIAL SURVEY TASKS |
ICAS2012-11.7.3 |
| Kok, M. |
LABORATORY TESTING OF INSECT
CONTAMINATION FOR LAMINAR FLOW APPLICATIONS USING AN INSECT-IMPACT TEST
FACILITY |
ICAS2012-3.4.4 |
| Kolesnikov, E. |
AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS2012-3.1.2 |
| Kölzsch, A. |
VORTEX FLOW MANIPULATION ON
GENERIC DELTA WING CONFIGURATIONS |
ICAS2012-3.6.4 |
| Kondakov, I. |
DESIGNING PRO-COMPOSITE
AIRCRAFT CONCEPTS AND LAYOUTS TO MAXIMIZE POTENTIAL BENEFITS OF HIGH SPECIFIC
STRENGTH OF CFRP |
ICAS2012-1.7.3 |
| Konno, A. |
MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1.ST2 |
| Kontis, K. |
EXPERIMENTAL STUDIES ON
MICRO-VORTEX GENERATORS IN HYPERSONIC FLOW |
ICAS2012-3.5.2 |
| Kontis, K. |
PERFORMANCE ANALYSIS OF A
SCRAMJET INLET-ISOLATOR USING EXPERIMENTAL & NUMERICAL METHODS |
ICAS2012-P4.12 |
| Kopylov, I. A. |
METHODS AND FACILITIES TO BE
USED TO EVALUATE THE AIRCRAFT FLIGHT AND NAVIGATION EQUIPMENT IN FLIGHT TESTS |
ICAS2012-5.6.3 |
| Korn, B. |
FLIGHT TESTING OF NOISE
ABATING RNP PROCEDURES AND STEEP APPROACHES |
ICAS2012-4.9.1 |
| Korovin, A. A. |
TECHNIQUE FOR FLYING
QUALITIES AND PIO PREDICTION |
ICAS2012-5.9.2 |
| Koshelenko, A. V. |
TECHNIQUE FOR FLYING
QUALITIES AND PIO PREDICTION |
ICAS2012-5.9.2 |
| Kosushkin, K. G. |
ADVANCED AEROSPACE SYSTEMS
WITH INTERCONTINENTAL AND GLOBAL RANGE OF FLIGHT |
ICAS2012-1.5.2 |
| Kouchi, T. |
EFFECT OF VENT MIXER TO
MIXING CHARACTERISTICS IN SUPERSONIC FLOW |
ICAS2012-P4.4 |
| Kovalev, I. E. |
ADVANCED AEROSPACE SYSTEMS
WITH INTERCONTINENTAL AND GLOBAL RANGE OF FLIGHT |
ICAS2012-1.5.2 |
| Kozakiewicz, A. |
A NEW APPROACH TO IDENTIFICATION AND OPTIMIZATION OF AIRFOILS
BY USING THE COMBINATORIAL-CYCLIC METHOD |
ICAS2012-P2.24 |
| Kozharinov, E.V. |
OPTIMAL HIGH-SPEED
HELICOPTER TRANSMISSION DESIGNS |
ICAS2012-P4.13 |
| Kozhemyako, P. G. |
EXPERIMENTAL AND NUMERICAL
STUDY OF TWO FIRST HIGHLY-LOADED STAGES OF COMPRESSORS AS A PART OF HPC AND
SEPARATE UNIT |
ICAS2012-4.6.1 |
| Krause, D. |
THE DEVELOPMENT OF PRODUCT
AND ASSEMBLY CONCEPTS FOR AIRCRAFT CABIN INTEGRATION |
ICAS2012-9.9.1 |
| Krombholz, C. |
IMPROVING THE PRODUCTION
QUALITY OF THE ADVANCED AUTOMATED FIBER PLACEMENT PROCESS BY MEANS OF ONLINE
PATH CORRECTION |
ICAS2012-6.1.3 |
| Kruchkov, A. N. |
THE INSTABILITY OF THE
PIPELINE DUE TO TRANSPORTING FLUID’S PRESSURE RIPPLES |
ICAS2012-8.11.1 |
| Krupa, V. G |
THE EXPERIENCE OF HIGH
PRESSURE RATIO SINGLE STAGE HPT DESIGNING |
ICAS2012-P4.15 |
| Krus, P. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
| Krus, P. |
AIRCRAFT SYSTEM SIMULATION
FOR PRELIMINARY DESIGN |
ICAS2012-1.9.3 |
| Krus, P. |
MORE ELECTRICAL
ENVIRONMENTAL CONTROL SYSTEM SIMULATION |
ICAS2012-6.6.4 |
| Kruse, M. |
MISSION AND ECONOMIC
ANALYSIS OF AIRCRAFT WITH NATURAL LAMINAR FLOW TECHNOLOGY |
ICAS2012-1.7.4 |
| Krzysiak, A. |
HELICOPTER RETREATING BLADE
STALL CONTROL USING SELF-SUPPLYING AIR JET VORTEX |
ICAS2012-3.6.2 |
| Kubo, D. |
TRANSITION FLIGHT OF QUAD
TILT WING VTOL UAV |
ICAS2012-11.1.3 |
| Kubo, D. |
HIGH ANGLE OF ATTACK FLIGHT
CONTROL OF A TAIL-SITTER UNMANNED AIRCRAFT |
ICAS2012-11.8.2 |
| Kubo, K. |
THEORETICAL AND EXPERIMENTAL
INVESTIGATIONS ON CHOKING PHENOMENA OF AXISYMMETRIC CONVERGENT NOZZLE FLOW |
ICAS2012-P2.11 |
| Kuenz, A. |
IMPLEMENTING TIME BASED CDA
OPERATIONS IN A MEDIUM-HIGH DENSITY ATM ENVIRONMENT |
ICAS2012-10.8.1 |
| Kufieta, K. |
OPTIMIZATION OF A NEW
MULTI-PURPOSE UAS FOR SCIENTIFIC APPLICATIONS USING AERODYNAMIC
RECONFIGURATION |
ICAS2012-11.6.4 |
| Kügler, D. |
FLIGHT TESTING OF NOISE
ABATING RNP PROCEDURES AND STEEP APPROACHES |
ICAS2012-4.9.1 |
| Kuhn, H. |
PROGRESS AND PERSPECTIVES OF
ELECTRIC AIR TRANSPORT |
ICAS2012-8.6.1 |
| Kuijk, J. van |
HOW A HIGH-SCHOOL STUDENT
BUILT THE FIRST DUTCH HUMAN POWERED AIRCRAFT |
ICAS2012-1.6.3 |
| Kunze, T. |
DYNAMIC TURNAROUND
MANAGEMENT IN A HIGHLY AUTOMATED AIRPORT ENVIRONMENT |
ICAS2012-10.9.2 |
| Kurdelski, M. |
FATIGUE LIFE ANALYSIS OF
MAIN LANDING GEAR PULL-ROD OF THE
FIGHTER JET AIRCRAFT |
ICAS2012-12.4.3 |
| Kurdelski, M. |
INTRODUCTION OF A STRUCTURE
INTEGRITY PROGRAM FOR A MILITARY TRAINER AIRCRAFT |
ICAS2012-12.6.2 |
| Kurdila, A. |
A
LEAP IN LEARNED BIO-INSPIRED FLIGHT |
ICAS2012-9.5.ST |
| Kurihara, J. |
AERODYNAMIC CHARACTERISTICS
OF A BIRD-LIKE ASSEMBLED WING |
ICAS2012-P2.22 |
| Kuzmina, S. I. |
ANALYSIS OF STATIC AND
DYNAMIC AEROELASTIC CHARACTERISTICS OF AIRPLANE IN TRANSONIC FLOW |
ICAS2012-8.10.4 |
| Kwak, D. |
NUMERICAL STUDY OF THE
REYNOLDS NUMBER EFFECT ON LOW ASPECT
RATIO WINGS AT LOW SPEED |
ICAS2012-2.10.2 |
| Kwak, D. |
STUDIES ON IMPROVEMENT OF
NONLINEAR PITCHING MOMENT CHARACTERISTICS OF CRANKED-ARROW WING |
ICAS2012-3.2.1 |
| Kwiek, A. |
MODULAR AEROPLANE SYSTEM. A
CONCEPT AND INITIAL INVESTIGATION |
ICAS2012-1.3.2 |
| Kwon, O. J. |
MODELING OF NO AND OH
INFRARED RADIATION ON A CONVERGENT-DIVERGENT NOZZLE |
ICAS2012-P4.6 |
| La Rocca, G. |
COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS2012-1.9.1 |
| La Rocca, G. |
THE DESIGN AND ENGINEERING
ENGINE. TOWARDS A MODULAR SYSTEM FOR COLLABORATIVE AIRCRAFT DESIGN |
ICAS2012-6.3.3 |
| la Rocca, G. |
AUTOMATIC FLATTENING OF THREE-DIMENSIONAL WIRING HARNESSES FOR
MANUFACTURING |
ICAS2012-6.4.2 |
| Labit, S. |
DERIVATED TURBULENCE MODEL
TO PREDICT HARMONIC LOADS IN TRANSONIC SEPARATED FLOWS OVER A BUMP |
ICAS2012-4.6.4 |
| Lahur, P. |
DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11.ST |
| Lahur, P. R. |
AUTOMATIC HANDLING OF
DEFECTIVE SURFACE GEOMETRY WITHIN GRID GENERATION FOR NAVIER-STOKES
COMPUTATION |
ICAS2012-2.11.1 |
| Lai, J. |
FLIGHT TRIAL OF AN
ELECTRO-OPTICAL SENSE-AND-AVOID SYSTEM |
ICAS2012-11.2.1 |
| Lai, J. |
FIELD-OF-VIEW, DETECTION
RANGE, AND FALSE ALARM TRADE-OFFS IN VISION-BASED AIRCRAFT DETECTION |
ICAS2012-6.9.1 |
| Lam, J. K.-W. |
COLD FUEL TEST RIG TO
INVESTIGATE ICE ACCRETION ON DIFFERENT PUMP INLET FILTER-MESH SCREENS |
ICAS2012-6.5.2 |
| Lambregts, A. A. |
FLY-BY-WIRE AUGMENTED MANUAL
CONTROL - BASIC DESIGN CONSIDERATIONS |
ICAS2012-5.4.1 |
| Langen, T. H. M. |
THE DESIGN AND ENGINEERING
ENGINE. TOWARDS A MODULAR SYSTEM FOR COLLABORATIVE AIRCRAFT DESIGN |
ICAS2012-6.3.3 |
| Langkamp, D. |
TETHERING
UNMANNED ROTORCRAFT FOR HIGH-ENDURANCE OPERATIONS |
ICAS2012-P1.3 |
| Lanzillo, G. |
DESIGN OF MASS SAVING
CONFIGURATIONS FOR WINGED REENTRY VEHICLES |
ICAS2012-1.5.3 |
| Larsson, R. |
NONLINEAR AERODYNAMIC
MODELING OF UNSTABLE AIRCRAFT USING FLIGHT TEST DATA |
ICAS2012-5.10.1 |
| Lau, F. J. P. |
ON SOUND GENERATION BY
MOVING SURFACES AND CONVECTED SOURCES IN A FLOW |
ICAS2012-P2.8 |
| Laurenzi, S. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
| Lawson, C. P. |
COLD FUEL TEST RIG TO
INVESTIGATE ICE ACCRETION ON DIFFERENT PUMP INLET FILTER-MESH SCREENS |
ICAS2012-6.5.2 |
| Lawson, C. P. |
TOWARDS TRAJECTORY
PREDICTION AND OPTIMISATION FOR ENERGY EFFICIENCY OF AN AIRCRAFT WITH
ELECTRICAL AND HYDRAULIC ACTUATION SYSTEMS |
ICAS2012-6.7.3 |
| Le Tallec, C. |
AIRCRAFT 4D CONTRACT BASED
OPERATION: THE 4DCO-GC PROJECT |
ICAS2012-10.3.3 |
| Le Tallec, C. |
A PERSONAL PLANE AIR
TRANSPORTATION SYSTEM: THE PPLANE PROJECT |
ICAS2012-10.5.1 |
| Ledogar, J. |
EOLE, AN INNOVATIVE FLYING
SCALE DEMONSTRATOR FOR AIR-LAUNCH-TO-ORBIT AUTOMATIC SYSTEMS |
ICAS2012-1.11.2 |
| Lee, C. H. |
DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS2012-10.4.1 |
| Lee, C. -H. |
AUTOPILOT DESIGN FOR AN
AGILE MISSILE USING L1 ADAPTIVE BACKSTEPPING CONTROL |
ICAS2012-P5.4 |
| Lee, D. S. |
ROBUST AERODYNAMIC DESIGN
OPTIMISATION OF MORPHING AEROFOIL/WING USING DISTRIBUTED MOGA |
ICAS2012-11.10.3 |
| Lee, I. |
AEROELASTIC ANALYSIS FOR
HELICOPTER ROTOR BLADES IN HOVER AND FORWARD FLIGHTS |
ICAS2012-11.5.3 |
| Lee, J. |
OPTIMIZATION OF
TWO-DIMENSIONAL WING IN GROUND EFFECT CONSIDERING AERODYNAMIC CENTRE OF
HEIGHT AND LIFT |
ICAS2012-P2.15 |
| Lee, J. W. |
AN INTEGRATED FRAMEWORK FOR
INNOVATIVE COMPOUND GYROPLANE DESIGN SYSTEM |
ICAS2012-1.4.ST |
| Lee, K. -J. |
VERIFICATION OF OPTICAL
PAYLOAD CFRP STRUCTURE FOR SATELLITE THROUGH ANALYSIS AND SPACE QUALIFICATION
TEST |
ICAS2012-P3.9 |
| Lee, M. |
EFFECT OF OFF-NORMAL LOADING
ON THE BOND STRENGTH MEASUREMENT OF BONDED REPAIRS |
ICAS2012-12.2.1 |
| Lee, S. -T. |
A METHOD FOR THE EVALUATION
OF ELECTROMECHANICAL ACTUATOR SYSTEMS USING EXERGY |
ICAS2012-6.6.3 |
| Lee, Y. J. |
AN INTEGRATED FRAMEWORK FOR
INNOVATIVE COMPOUND GYROPLANE DESIGN SYSTEM |
ICAS2012-1.4.ST |
| Lefebvre, T. |
AIRCRAFT CONCEPTUAL DESIGN
IN A MULTI-LEVEL, MULTI-FIDELITY, MULTI-DISCIPLINARY OPTIMIZATION PROCESS |
ICAS2012-1.6.4 |
| Lehmkuehler, K. |
DESIGN AND TEST OF A UAV
BLENDED WING BODY CONFIGURATION |
ICAS2012-1.8.3 |
| Lehner, S. |
MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS2012-6.4.1 |
| Lei, W. |
MULTI-OBJECTIVE AERODYNAMIC
OPTIMIZATION DESIGN OF MULTI-ELEMENT AIRFOIL USING KRIGING MODEL |
ICAS2012-2.3.ST |
| Leipold, A. |
ICAO’S BALANCED APPROACH TO
NOISE MANAGEMENT AND ITS INFLUENCE ON THE ECONOMIC IMPACT OF AIR
TRANSPORTATION |
ICAS2012-7.10.4 |
| Lemmens, Y. |
DESIGN STUDY OF AN ACTIVE
GURNEY FLAP SYSTEM FOR HELICOPTER ROTOR BLADES |
ICAS2012-6.11.1 |
| Lemmens, Y. |
IDENTIFICATION OF HELICOPTER
GROUND RESONANCE WITH MULTI-BODY SIMULATION |
ICAS2012-8.3.2 |
| Lemmens, Y. |
RELIABILITY ANALYSIS OF
AIRCRAFT SYSTEM ARCHITECTURES |
ICAS2012-P9.1 |
| Leski, A. |
FATIGUE LIFE ANALYSIS OF
MAIN LANDING GEAR PULL-ROD OF THE
FIGHTER JET AIRCRAFT |
ICAS2012-12.4.3 |
| Leski, A. |
INTRODUCTION OF A STRUCTURE
INTEGRITY PROGRAM FOR A MILITARY TRAINER AIRCRAFT |
ICAS2012-12.6.2 |
| Lesser, A. |
NUMERICAL INVESTIGATION OF
THE EFFECT OF INFLOW DISTORTIONS ON TRANSONIC AXIAL COMPRESSOR STAGES WITH 2D
AND 3D CALCULATIONS |
ICAS2012-4.6.2 |
| Levandowski, C. P. |
ROBUST LIFECYCLE
OPTIMIZATION OF TURBINE COMPONENTS USING SIMULATION PLATFORMS |
ICAS2012-4.3.2 |
| Levinski, O. |
APPLICATION OF DYNAMIC
PRESSURE MEASUREMENT FOR EMPENNAGE BUFFET |
ICAS2012-3.4.1 |
| Levora, T. |
ADVANCED DISPLAY AND
POSITION ANGLES MEASUREMENT SYSTEMS |
ICAS2012-P6.3 |
| Lewe, J. -H. |
A METHOD FOR THE EVALUATION
OF ELECTROMECHANICAL ACTUATOR SYSTEMS USING EXERGY |
ICAS2012-6.6.3 |
| Li, D. |
IMPROVED PARTICLE SWARM
OPTIMIZATION BASED ON SOCIAL MODEL FOR AERODYNAMIC DESIGN |
ICAS2012-11.10.4 |
| Li, D. |
NUMERICAL INVESTIGATION OF
FLOW OVER MULTI-ELEMENT AIRFOILS WITH LIFT-ENHANCING TABS |
ICAS2012-2.3.2 |
| Li, D. |
NUMERICAL STUDY OF PITCHING
OSCILLATION EFFECT ON AERODYNAMIC CHARACTERISTICS OVER ASYMMETRIC VORTEX
STRUCTURE OF SLENDER REVOLUTION |
ICAS2012-2.5.2 |
| Li, G. |
RESEARCH ON FAILURE
SIMULATION OF CIVIL AIRCRAFT FLIGHT MANAGEMENT SYSTEM |
ICAS2012-5.6.4 |
| Li, H. |
A NEW APPROACH FOR RE-ENTRY
VEHICLE TRAJECTORY PLANNING AND GUIDANCE |
ICAS2012-5.7.5 |
| Li, H. |
THE GLARE EVALUATION METHOD
FOR CIVIL AIRPLANE FLIGHT DECK |
ICAS2012-9.3.3 |
| Li, H. |
MANEUVERING TARGET TRACKING
BASED ON THE EKF |
ICAS2012-P5.2 |
| Li, J. |
INVESTIGATION
ON PROPELLER ENGINE OPTIMUM INSTALLATION POSITION ON A SOLAR POWERED UNMANNED
AERIAL VEHICLE |
ICAS2012-2.10.5 |
| Li, J. |
EXPLORING
THE AERODYNAMIC INTERFERENCE OF PROPELLER-WING ON A SOLAR POWERED UNMANNED
AERIAL VEHICLE |
ICAS2012-9.8.3 |
| Li, L. |
INFLUENCE OF FLAPPING WING
UNSTEADY MOTION ON AERODYNAMIC PERFORMANCE OF HORIZONTAL TAIL |
ICAS2012-2.7.5 |
| Li, M. |
ENHANCING THE "LAST
MILE" COMMUNICATIONS AT AIRPORTS |
ICAS2012-10.10.5 |
| Li, W. |
PRELIMINARY STUDY OF EMA
LANDING GEAR ACTUATION |
ICAS2012-6.8.2 |
| Li, Y. |
NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS2012-2.3.3 |
| Li, Y. |
LCF BEHAVIOR AND LIFE
EVALUATION OF A SINGLE CRYSTAL NICKEL BASE SUPERALLOY UNDER DIFFERENT DWELL
CONDITION |
ICAS2012-7.3.3 |
| Li, Y. |
STRUCTURAL
INTEGRITY ANALYSIS AND TEST OF FATIGUE CRITICAL LOCATION OF MA60 REGIONAL JET |
ICAS2012-7.9.4 |
| Li, Z. |
CHARACTERISTICS
OF AN 80-DEG SWEPT DELTA WING IN WING ROCK OR FREE YAWING |
ICAS2012-3.1.ST1 |
| Li, Z. |
RESEARCH ON FAILURE
SIMULATION OF CIVIL AIRCRAFT FLIGHT MANAGEMENT SYSTEM |
ICAS2012-5.6.4 |
| Li, Z. |
A GENERAL FOOTPRINT
GENERATION APPROACH FOR LIFTING RE-ENTRY VEHICLE |
ICAS2012-5.7.2 |
| Li, Z. |
ANGLE OF ATTACK OPERATION
ZONE ANALYSIS AND DESIGN FOR LIFTING ENTRY |
ICAS2012-5.7.3 |
| Li, Z. |
A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
| Liao, M. |
PROBABILISTIC RISK ANALYSIS
FOR AIRCRAFT STRUCTURES WITH LIMITED IN-SERVICE DAMAGES |
ICAS2012-7.9.3 |
| Liao, Y. |
ANGLE OF ATTACK OPERATION
ZONE ANALYSIS AND DESIGN FOR LIFTING ENTRY |
ICAS2012-5.7.3 |
| Liauzun, C. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
| Liebers, N. |
SENSOR AND
REAL-TIME-PROCESS-SIMULATION GUIDED AUTOCLAVE PROCESS CONTROL FOR COMPOSITE
PRODUCTION |
ICAS2012-6.1.2 |
| Lieser, J. |
IMPROVED MODELLING OF
VORTICAL MIXING FOR THE SIMULATION OF EFFICIENT PROPULSION SYSTEMS |
ICAS2012-4.10.1 |
| Liew, K. E. |
PRODUCTION
OF BIO-FUEL FROM ALGAE BIOMASS, NANNOCHLOROPSIS OCULATA, FOR ADDITION TO
KEROSENE JET A-1 |
ICAS2012-8.6.4 |
| Lim, D. |
DESIGN OF UNMANNED AIR
SYSTEMS FOR USE IN SEARCH AND RESCUE IN THE NORTH ATLANTIC |
ICAS2012-9.9.3 |
| Lim, D. W. |
METHODOLOGY FOR THE DESIGN
OF UNMANNED AIRCRAFT PRODUCT FAMILIES |
ICAS2012-9.9.2 |
| Lim, S. H. |
A FEASIBILITY STUDY FOR
MULTI-MATERIAL RETROFITTABLE ENERGY ABSORBING STRUCTURE FOR AGED HELICOPTER
SUBFLOOR |
ICAS2012-12.3.3 |
| Lim, S. H. |
DIRECTIONAL ENHANCEMENT OF
COMPOSITE STRUCTURES ENERGY ABSORPTION USING MAGNETORHEOLOGICAL FLUIDS |
ICAS2012-7.8.1 |
| Lim, S. H. |
EXPERIMENTAL DEVELOPMENT AND
ANALYSIS OF AN ACTIVE CRUSHING ELEMENT USING PRESSURIZED COMPOSITE TUBES |
ICAS2012-8.1.ST |
| Lim, S.-H. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
| Lin, P. |
CONTROL-ORIENTED MODELING
AND ANALYSIS OF AERO-THERMO-ELASTIC-PROPULSION HYPERSONIC VEHICLE |
ICAS2012-1.5.1 |
| Linde, P. |
ASSESSMENT OF STRUCTURAL
EFFECT OF SELECTIVE STITCHING ON COMPOSITE SKIN-STIFFENER BONDING |
ICAS2012-8.9.1 |
| Linke, F. |
MISSION AND ECONOMIC
ANALYSIS OF AIRCRAFT WITH NATURAL LAMINAR FLOW TECHNOLOGY |
ICAS2012-1.7.4 |
| Liu, C. K |
ENGINEERING FAILURE MODES
AND FRACTURE CHARACTERISTICS OF SINGLE CRYSTAL SUPERALLOY BLADES |
ICAS2012-4.2.ST |
| Liu, C. K. |
FRACTURE
ANALYSIS OF BLADE DOVETAIL OF TC11 TITANIUM ALLOY |
ICAS2012-P4.7 |
| Liu, D. -B. |
THE FABRICATION AND
CHARACTERIZATION OF TiO2 UV DETECTOR |
ICAS2012-7.3.ST |
| Liu, G. |
CHARACTERISTICS
OF AN 80-DEG SWEPT DELTA WING IN WING ROCK OR FREE YAWING |
ICAS2012-3.1.ST1 |
| Liu, G. Z. |
FLOW
CONTROL TEST RESEARCH OF AIRCRAFT MODEL WITH ADJUSTABLE CANAEDS |
ICAS2012-P2.5 |
| Liu, H. -Y. |
NUMERICAL STUDY ON RESIDUAL
THERMAL STRESSES IN CARBON FIBRE PULLOUT |
ICAS2012-7.3.1 |
| Liu, J. |
COMPARISON OF INFILL
SAMPLING CRITERIA IN KRIGING-BASED AERODYNAMIC OPTIMIZATION |
ICAS2012-11.10.ST |
| Liu, J. |
DESIGN OF LAMINAR
SUPERCRITICAL AIRFOILS BASED ON NAVIER-STOKES EQUATIONS |
ICAS2012-2.2.2 |
| Liu, J. |
LAMINAR FLOW WING’S
OPTIMIZATION DESIGN BY RANS SOLVER WITH AUTOMATIC TRANSITION PREDICTION |
ICAS2012-2.2.3 |
| Liu, L. |
THE
NUMERICAL SIMULATION OF BIRD STRIKE ON BLADES OF AN ENGINE |
ICAS2012-4.4.3 |
| Liu, Q. |
MICROSTRUCTURE AND
MECHANICAL PROPERTIES OF LASER CLADDING REPAIR OF AISI 4340 STEEL |
ICAS2012-12.4.4 |
| Liu, W. |
STUDY ON THE FLOW STRUCTURES
OF THE SHOCKWAVE AND TURBULENT BOUNDARY-LAYER INTERACTION |
ICAS2012-11.4.3 |
| Liu, Y. |
CONTROL ALLOCATION FOR
AIRCRAFTS WITH MULTIPLE CONTROL EFFECTORS DURING TAKEOFF AND LANDING PHASES |
ICAS2012-5.3.3 |
| Loader, C. |
INITIAL RESULTS FROM DSTO’S
CORROSION STRUCTURAL INTEGRITY ROADMAP |
ICAS2012-12.6.1 |
| Lobentanzer, H. |
VOLTAIR - THE ALL ELECTRIC
PROPULSION CONCEPT PLATFORM – A VISION FOR ATMOSPHERIC FRIENDLY FLIGHT |
ICAS2012-4.7.2 |
| Lööf, J. |
ROBUST LIFECYCLE
OPTIMIZATION OF TURBINE COMPONENTS USING SIMULATION PLATFORMS |
ICAS2012-4.3.2 |
| Lorenz, L. |
PROGRESS AND PERSPECTIVES OF
ELECTRIC AIR TRANSPORT |
ICAS2012-8.6.1 |
| Loth, S. |
THE EREA VISION ON HIGH
PRIORITY RESEARCH AXES TOWARDS AIR TRANSPORT SYSTEM 2050 |
ICAS2012-1.7.1 |
| Love, J. |
DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS2012-10.4.1 |
| Lowe, A. |
A METHOD FOR THE EVALUATION
OF ELECTROMECHANICAL ACTUATOR SYSTEMS USING EXERGY |
ICAS2012-6.6.3 |
| Lowenberg, M. H. |
COMPUTATIONAL AND
EXPERIMENTAL ANALYSIS OF THE ACTIVE MORPHING WING CONCEPT |
ICAS2012-2.5.3 |
| Lu, G. |
THE INTEGRATION METHOD OF
FAULT DIAGNOSIS AND HEALTH ASSESSMENT FOR UAV SYSTEM |
ICAS2012-12.1.3 |
| Lu, H. Y. |
STUDY OF THE PRESSURE DROP
FOR RADIAL INFLOW BETWEEN CO-ROTATING DISCS |
ICAS2012-4.4.ST |
| Lu, Y. L |
A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
| Luber, W. G. |
AEROSERVOELASTIC FLIGHT CONTROL DESIGN FOR A MILITARY COMBAT AIRCRAFT WEAPON SYSTEM |
ICAS2012-5.4.2 |
| Lucchi, F. |
INNOVATION IN MAN MACHINE
INTERFACES: USE OF 3D CONFORMAL SYMBOLS IN THE DESIGN OF FUTURE HUDS (HEAD UP
DISPLAYS) |
ICAS2012-9.7.2 |
| Lukovnikov, A. V. |
STUDIES
OF PROPULSION SYSTEM CONCEPTS FOR ADVANCED SUBSONIC AIRLINERS |
ICAS2012-4.7.3 |
| Lukyanov, A. V. |
DEVELOPMENT OF THE AUTOMATED
SYSTEM ON THE BASIS OF NEURAL NETWORKS FOR FLIGHT SAFETY OF AIRCRAFT |
ICAS2012-5.2.2 |
| Lunsdström, D. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
| Luo, X. |
STUDY OF THE PRESSURE DROP
FOR RADIAL INFLOW BETWEEN CO-ROTATING DISCS |
ICAS2012-4.4.ST |
| Lwin, T. |
AN INTEGRATED FRAMEWORK FOR
INNOVATIVE COMPOUND GYROPLANE DESIGN SYSTEM |
ICAS2012-1.4.ST |
| Lyubimov, D. |
EXPERIMENTAL AND NUMERICAL
RESEARCH OF UNSTEADY FLOW IN CURVILINEAR CHANNEL WITH ACTIVE FLOW MANAGEMENT
USING “SYNTHETIC” JETS |
ICAS2012-4.4.2 |
| Ma, J. G. |
RESEARCH ON AIRBORNE
INTELLIGENT HYDRAULIC PUMP SYSTEM |
ICAS2012-6.10.3 |
| Ma, W. |
A MICRO-SIMULATION OF
AIRPORT PASSENGERS WITH ADVANCED TRAITS |
ICAS2012-10.9.4 |
| Ma, Z. |
THE GLARE EVALUATION METHOD
FOR CIVIL AIRPLANE FLIGHT DECK |
ICAS2012-9.3.3 |
| Maas, R. |
BUCKLING-OPTIMIZED VARIABLE
STIFFNESS LAMINATES FOR A COMPOSITE FUSELAGE WINDOW SECTION |
ICAS2012-8.9.3 |
| Machunze, W. |
DESIGN, ANALYSIS AND
MANUFACTURING OF A THERMOPLASTIC UD CF-PEEK SLAT |
ICAS2012-6.1.1 |
| Magerramova, L. |
ACHIEVEMENT OF BIMETALLIC
BLISKS INTEGRATED DISSIMILAR ALLOYS FOR PROMISING HIGH TEMPERATURE AVIATION
GAS TURBINE ENGINES |
ICAS2012-4.1.3 |
| Magerramova, L. A. |
INTERDISCIPLINARY COMPLEX
DESIGN OF MODERN HIGH AND LOW PRESSURE TURBINES |
ICAS2012-4.3.3 |
| Makarov, A. |
EXPERIMENTAL AND NUMERICAL
RESEARCH OF UNSTEADY FLOW IN CURVILINEAR CHANNEL WITH ACTIVE FLOW MANAGEMENT
USING “SYNTHETIC” JETS |
ICAS2012-4.4.2 |
| Makaryants, G. M. |
THE INSTABILITY OF THE
PIPELINE DUE TO TRANSPORTING FLUID’S PRESSURE RIPPLES |
ICAS2012-8.11.1 |
| Malinin, V. V. |
NUMERICAL MODELING OF FLOW
IN GASDYNAMIC RESONATOR AND MODEL VALIDATION BY RESULTS OF PULSE ENGINE TESTS |
ICAS2012-P4.10 |
| Malis, M. |
THE CFRP SAILPLANE WING
SEGMENTS MANUFACTURED BY FILAMENT PLACEMENT |
ICAS2012-7.5.ST |
| Malm, A. M. |
MODEL BASED DEFINITION
WITHIN RELOCATION OF AIRCRAFT PRODUCTION |
ICAS2012-9.9.4 |
| Mandanis, G. |
SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS2012-10.6.1 |
| Mane, M. |
DESCRIPTION AND EVALUATION
OF MULTI-THREAT TRACKING ARCHITECTURES |
ICAS2012-11.2.3 |
| Mangion, D. Z. |
RUNWAY CONFLICT ALERTING
DURING TAKE-OFF AND LANDING: ADVISORY OR DIRECTIVE? |
ICAS2012-9.10.1 |
| Maphanga, S. |
A PRACTICAL, ROUTE-BASED
APPROACH TO AIRSPACE CAPACITY MANAGEMENT |
ICAS2012-10.2.2 |
| Maqsood, A. |
FLEXIBLE WING AERODYNAMICS
AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.1 |
| Maqsood, A. |
EXPERIMENTAL INVESTIGATION
OF A BI-PLANE MICRO AIR VEHICLE |
ICAS2012-3.3.4 |
| Marchetti, M. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
| Mare, J. -C. |
COUPLING MECH. & THERMAL
MODELS IN PRELIMINARY DESIGN OF POWER TRANSMISSIONS DRIVEN BY THERMAL ISSUES |
ICAS2012-6.6.1 |
| Mare, J. -C. |
INVESTIGATION IN THE DYNAMIC
FORCE EQUALIZATION OF DISSIMILAR REDUNDANT ACTUATION SYSTEMS OPERATING IN
ACTIVE/ACTIVE MODE |
ICAS2012-6.8.1 |
| Marguet, S. |
POSTBUCKLING COMPUTATION OF
LARGE STIFFENED STRUCTURES |
ICAS2012-8.1.3 |
| Marino, M. |
THE INFLUENCE OF TURBULENCE
INTENSITY ON THE FLOW STRUCTURE OVER A THIN AIRFOIL AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.2 |
| Marino, M. |
OPTIMUM LOCATION OF PRESSURE
MEASUREMENTS AROUND A WING AS A DYNAMIC CONTROL INPUT IN SMOOTH AND TURBULENT
CONDITIONS |
ICAS2012-3.3.3 |
| Markwart, M. |
EVALUATION OF CABIN
DISPLACEMENT VENTILATION UNDER FLIGHT CONDITIONS |
ICAS2012-6.10.2 |
| Marques, J. M. G. |
A PROBABILITY ASSESSMENT OF
THE FLIGHT SAFETY RELEVANT TO COLLISION AVOIDANCE |
ICAS2012-10.7.5 |
| Marshall, D. D. |
BEYOND TWO-EQUATION
TURBULENCE MODELING FOR THE REYNOLDS-AVERAGED NAVIER-STOKES EQUATIONS:
ADVANCES IN COMPLEX FLOW PREDICTIONS |
ICAS2012-2.4.1 |
| Marta, A. C. |
ANALYTICAL NATURAL
FREQUENCIES OF TAPERED WINGS |
ICAS2012-P3.2 |
| Martensson, H. |
CFD OPTIMIZATION OF A
TRANSONIC COMPRESSOR USING MULTIOBJECTIVE GA AND METAMODELS |
ICAS2012-4.6.3 |
| Martin, E. L. |
DEVELOPMENT OF AN
EXPERIMENTAL TECHNIQUE FOR HIGH TEMPERATURE IMPINGEMENT STUDIES |
ICAS2012-12.6.3 |
| Martin, L. |
RESOLVING OFF-NOMINAL
SITUATIONS IN SCHEDULE-BASED TERMINAL AREA OPERATIONS: RESULTS FROM A
HUMAN-IN-THE-LOOP SIMULATION |
ICAS2012-10.5.2 |
| Martinez, G. |
THE EREA VISION ON HIGH
PRIORITY RESEARCH AXES TOWARDS AIR TRANSPORT SYSTEM 2050 |
ICAS2012-1.7.1 |
| Martínez, M. |
PRELIMINARY AERODYNAMIC
INVESTIGATION OF AN UNMANNED BOX-WING AIRCRAFT |
ICAS2012-P2.13 |
| Martínez-Val, R. |
CARRIER SUITABILITY OF
LAND-BASED AIRCRAFT |
ICAS2012-1.1.ST |
| Mason, M. |
THE AFFECT OF SCREEN SIZE ON
MISSION COMMANDER’S SITUATION AWARENESS |
ICAS2012-9.7.5 |
| Masson, B. |
ENGINE-OUT TAKEOFF PATH
OPTIMIZATION OUT OF TERRAIN CHALLENGING AIRPORTS |
ICAS2012-5.8.2 |
| Masuya, G. |
EFFECT OF VENT MIXER TO
MIXING CHARACTERISTICS IN SUPERSONIC FLOW |
ICAS2012-P4.4 |
| Mateescu, D. |
STEADY
AND UNSTEADY FLOWS PAST AIRFOILS AT LOW REYNOLDS NUMBERS IN THE PROXIMITY OF
THE GROUND |
ICAS2012-3.6.ST |
| Mateják, V. |
THE DETERMINATION OF
DELAMINATION STRAIN ENERGY RELEASE RATE OF COMPOSITE BI-MATERIAL INTERFACE |
ICAS2012-7.4.1 |
| Matsuda, Y. |
EXPERIMENTAL STUDY OF THE
MORPHING FLAP AS A LOW NOISE HIGH LIFT DEVICE FOR AIRCRAFT WING |
ICAS2012-9.11.3 |
| Matsuno, T. |
ANALYTIC METHOD FOR FLIGHT
MOTION OF AIRCRAFT WITH A SINGLE VIDEO CAMERA AND ITS APPLICATION TO A FREE
FLIGHT GLIDER |
ICAS2012-5.6.1 |
| Matsuo, Y. |
NUMERICAL STUDY OF THE
EFFECTS OF CROSS-WIND ON THE JET BLAST DEFORMATION |
ICAS2012-10.10.3 |
| Matsushima, K. |
DEVELOPMENT OF SUPERSONIC
NATURAL LAMINAR FLOW WING DESIGN SYSTEM USING CFD-BASED INVERSE METHOD |
ICAS2012-2.2.1 |
| Matthews, N. |
SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS2012-7.2.2 |
| Mavris, D. |
STATISTICAL STABILITY AND
CONTROL ANALYSIS TO INVESTIGATE THE CONTROL EFFORT OF IMPROVING HANDLING
QUALITY CHARACTERISTICS |
ICAS2012-5.9.1 |
| Mavris, D. |
A METHOD FOR THE EVALUATION
OF ELECTROMECHANICAL ACTUATOR SYSTEMS USING EXERGY |
ICAS2012-6.6.3 |
| Mavris, D. |
DESIGN OF UNMANNED AIR
SYSTEMS FOR USE IN SEARCH AND RESCUE IN THE NORTH ATLANTIC |
ICAS2012-9.9.3 |
| Mavris, D. N. |
A COMPETITIVE AND
REAL-OPTIONS FRAMEWORK FOR THE ECONOMIC ANALYSIS OF LARGE AEROSPACE PROGRAMS |
ICAS2012-6.3.2 |
| Mavris, D. N. |
A NON-WEIGHT BASED,
MANUFACTURING INFLUENCED DESIGN (MIND) METHODOLOGY FOR PRELIMINARY DESIGN |
ICAS2012-6.4.3 |
| Mavris, D. N. |
A METHODOLOGY FOR PARAMETRIC
PRODUCTION PLANNING IN PRELIMINARY AIRCRAFT DESIGN |
ICAS2012-6.4.4 |
| Mavris, D. N. |
METHODOLOGY FOR THE DESIGN
OF UNMANNED AIRCRAFT PRODUCT FAMILIES |
ICAS2012-9.9.2 |
| Mavris, D. N. |
EVALUATING FLEXIBILITY IN
AIRPORT CAPACITY-ENHANCING TECHNOLOGY INVESTMENTS |
ICAS2012-P8.2 |
| Maximov, A. A. |
STUDIES
OF PROPULSION SYSTEM CONCEPTS FOR ADVANCED SUBSONIC AIRLINERS |
ICAS2012-4.7.3 |
| Mayes, P. |
EFFECTIVE SAFETY MANAGEMENT
SYSTEMS FOR ACCIDENT PREVENTION |
ICAS2012-9.10.2 |
| McCann, H. M. |
VIBRATION AND AEROELASTIC CLEARANCE WORK FOR JASSM INTEGRATION ONTO THE F/A-18A/B |
ICAS2012-8.10.3 |
| McCarthy, J. M. |
FLOW-INDUCED FLUTTER OF
SLENDER CANTILEVER HIGH-COMPLIANCE PLATES |
ICAS2012-8.10.5 |
| McDonald, M. |
QUANTITATIVE FRACTOGRAPHY
MARKERS FOR DETERMINING FATIGUE CRACK GROWTH RATES IN ALUMINIUM AND TITANIUM
AIRCRAFT STRUCTURES |
ICAS2012-12.4.1 |
| Mcfadyen, A. D. |
VISUAL SERVOING APPROACH TO
COLLISION AVOIDANCE FOR AIRCRAFT |
ICAS2012-11.3.1 |
| McIntyre, T. J. |
STUDY OF RADIATIVE HEAT
TRANSFER IN TITAN ATMOSPHERIC ENTRY |
ICAS2012-3.8.3 |
| McLeod, J. E. |
BI-AXIAL VIBRATION ENERGY
HARVESTING FOR USE ON AEROSPACE PLATFORMS |
ICAS2012-6.7.1 |
| McMullan, W. A. |
STREAMWISE AND CROSSFLOW
INSTABILITIES ON INCLINED CIRCULAR CYLINDERS |
ICAS2012-3.10.2 |
| McNally, D. |
DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS2012-10.4.1 |
| Medford, C. M. |
WATER TUNNEL FORCE AND
MOMENT STUDIES OF A MANEUVERING UCAV 1303 AND THEIR CONTROL |
ICAS2012-3.1.3 |
| Medici, G. |
INTEROPERABILITY OF MILITARY
AIRCRAFT VERSUS FUTURE AIR NAVIGATION SYSTEM (FANS) |
ICAS2012-10.1.3 |
| Medici, G. |
TURBOJET ANALYTICAL MODEL
DEVELOPMENT AND VALIDATION |
ICAS2012-4.10.5 |
| Mejias, L. |
FLIGHT TRIAL OF AN
ELECTRO-OPTICAL SENSE-AND-AVOID SYSTEM |
ICAS2012-11.2.1 |
| Mejias, L. |
FIELD-OF-VIEW, DETECTION
RANGE, AND FALSE ALARM TRADE-OFFS IN VISION-BASED AIRCRAFT DETECTION |
ICAS2012-6.9.1 |
| Mejias, L. A. |
VISUAL SERVOING APPROACH TO
COLLISION AVOIDANCE FOR AIRCRAFT |
ICAS2012-11.3.1 |
| Melin, T. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
| Melin, T. |
DESIGN OF UNMANNED AIR
SYSTEMS FOR USE IN SEARCH AND RESCUE IN THE NORTH ATLANTIC |
ICAS2012-9.9.3 |
| Meng, P. |
MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS2012-6.4.1 |
| Mercer, J. |
RESOLVING OFF-NOMINAL
SITUATIONS IN SCHEDULE-BASED TERMINAL AREA OPERATIONS: RESULTS FROM A
HUMAN-IN-THE-LOOP SIMULATION |
ICAS2012-10.5.2 |
| Metkemeijer, R. |
APACHE : INTEGRATED HYBRID
FUEL CELL SYSTEM FOR 2-SEAT ALL ELECTRIC AIRCRAFTS PROPULSION |
ICAS2012-6.7.4 |
| Micallef, M. |
A PROPOSAL FOR REVISED
APPROACHES AND PROCEDURES TO MALTA INTERNATIONAL AIRPORT |
ICAS2012-4.9.3 |
| Mieloszyk, J. |
MADO – SOFTWARE PACKAGE FOR
HIGH ORDER MULTIDISCIPLINARY AIRCRAFT
DESIGN AND OPTIMIZATION |
ICAS2012-1.9.4 |
| Mieloszyk, J. |
RESULTS OF THE GUST
RESISTANT MAV PROGRAMME |
ICAS2012-3.1.1 |
| Mieszalski, D. |
MADO – SOFTWARE PACKAGE FOR
HIGH ORDER MULTIDISCIPLINARY AIRCRAFT
DESIGN AND OPTIMIZATION |
ICAS2012-1.9.4 |
| Mikhaylov, S. V. |
AN EXPERIENCE OF USING
NUMERICAL METHODS IN EXPERIMENTAL INVESTIGATIONS OF TsAGI |
ICAS2012-P2.6 |
| Miki, H. |
PERFORMANCE EVALUATION OF A
BOUNDARY-LAYER DIVERTER FOR SUPERSONIC PROPULSION SYSTEM |
ICAS2012-6.2.2 |
| Milanese, A. |
EXPERIMENTAL AND NUMERICAL
ASSESSMENT OF HELICOPTER SUBFLOOR CRASHWORTHINESS |
ICAS2012-8.1.1 |
| Milanese, A. |
PRELIMINARY INVESTIGATION ON
THE FEASIBILITY OF A BIRD SURROGATE FOR FULL-SCALE BIRD IMPACT TEST |
ICAS2012-8.3.1 |
| Mileshin, V. |
STUDY ON NOISE OF COUNTER
ROTATING FAN MODELS AT CIAM ANECHOIC CHAMBER |
ICAS2012-3.9.4 |
| Mileshin, V. I. |
EXPERIMENTAL AND NUMERICAL
STUDY OF TWO FIRST HIGHLY-LOADED STAGES OF COMPRESSORS AS A PART OF HPC AND
SEPARATE UNIT |
ICAS2012-4.6.1 |
| Minaeifard, F. |
AN
OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES |
ICAS2012-6.5.ST |
| Minami, Y. |
AUTOPILOT
DESIGN FOR THE EOLE DEMONSTRATOR |
ICAS2012-5.3.4 |
| Minato, R. |
DEVELOPMENT OF A SMALL-SCALE
SUPERSONIC FLIGHT EXPERIMENT VEHICLE AS A FLYING TEST BED |
ICAS2012-1.2.2 |
| Mirkov, N. |
MANEUVERABILITY OF AN UAV
WITH COANDA EFFECT BASED LIFT PRODUCTION |
ICAS2012-P2.18 |
| Mirzaei, M. |
AN
OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES |
ICAS2012-6.5.ST |
| Mirzoyan, A. |
STUDIES ON REQUIRED
PERFORMANCES OF ADVANCED SUPERSONIC CIVIL AIRCRAFT AND THEIR PROPULSION
SYSTEMS FOR 2020-2035 TIMEFRAME |
ICAS2012-4.7.4 |
| Mirzoyan, L. |
STUDIES ON REQUIRED
PERFORMANCES OF ADVANCED SUPERSONIC CIVIL AIRCRAFT AND THEIR PROPULSION
SYSTEMS FOR 2020-2035 TIMEFRAME |
ICAS2012-4.7.4 |
| Mitchell, T. M. |
ENHANCING THE "LAST
MILE" COMMUNICATIONS AT AIRPORTS |
ICAS2012-10.10.5 |
| Miura, T. |
ANALYTIC METHOD FOR FLIGHT
MOTION OF AIRCRAFT WITH A SINGLE VIDEO CAMERA AND ITS APPLICATION TO A FREE
FLIGHT GLIDER |
ICAS2012-5.6.1 |
| Miyaji, K. |
FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS2012-5.2.1 |
| Miyatsu, Y. |
A BASIC STUDY ON EFFICIENCY IN JAPANESE
AIRSPACE |
ICAS2012-10.2.1 |
| Miyazato, Y. |
THEORETICAL AND EXPERIMENTAL
INVESTIGATIONS ON CHOKING PHENOMENA OF AXISYMMETRIC CONVERGENT NOZZLE FLOW |
ICAS2012-P2.11 |
| Miyazawa, Y. |
FLIGHT TRAJECTORY
OPTIMIZATION FOR AN EFFICIENT AIR TRANSPORTATION SYSTEM |
ICAS2012-5.8.3 |
| Mizobata, K. |
DEVELOPMENT OF A SMALL-SCALE
SUPERSONIC FLIGHT EXPERIMENT VEHICLE AS A FLYING TEST BED |
ICAS2012-1.2.2 |
| Mizukaki, T. |
INSTABILITY CHARACTERISTICS
OF SHOCK WAVES AHEAD OF A HEMISPHERICAL SHELL AT SUPERSONIC SPEEDS |
ICAS2012-11.4.2 |
| Mizukaki, T. |
VISUALIZATION OF UNSTEADY
BEHAVIOR OF SHOCK WAVES AROUND SUPERSONIC INTAKE INSTALLED IN SHOCK TUNNEL |
ICAS2012-P4.5 |
| Mohammadi-Amin, M. |
NONLINEAR AEROELASTIC
ANALYSIS OF SWEPT WINGS IN COMPRESSIBLE FLOW VIA THE HARMONIC BALANCE METHOD |
ICAS2012-8.7.1 |
| Mohseni Shakib, S. M. |
POST-BUCKLING
BEHAVIOR AND PROPAGATION OF DELAMINATION FOR COMPOSITE PANELS IN DIFFERENT
DELAMINATION SIZES |
ICAS2012-7.9.ST |
| Mohseni Shakib, S. M. |
BUCKLING
AND POST-BUCKLING RESPONSES OF SQUARE LAMINATE WITH VARIOUS SHAPED CUTOUTS
UNDER DIFFERENT LOADINGS |
ICAS2012-P3.7 |
| Molent, L. |
INVESTIGATION OF AN
IN-SERVICE CRACK SUBJECTED TO AERODYNAMIC BUFFET AND MANOEUVRE LOADS AND
EXPOSED TO AN CORROSIVE ENVIRONMENT |
ICAS2012-7.9.1 |
| Mollaei, F. |
FINDING TUNING FREQUENCY OF
SYMMETRIC AND ANTI-SYMMETRIC LAMB WAVES USING FEM |
ICAS2012-P3.6 |
| Mollwitz, V. |
FLIGHT TESTING OF NOISE
ABATING RNP PROCEDURES AND STEEP APPROACHES |
ICAS2012-4.9.1 |
| Momeni Massouleh, S. H. |
APPLICATION
OF SINGULAR VALUE DECOMPOSITION IN COMPONENT MODE SYNTHESIS WITH EXPERIMENTAL
APPROACH |
ICAS2012-8.11.3 |
| Montrucchio, C. |
INTEROPERABILITY OF MILITARY
AIRCRAFT VERSUS FUTURE AIR NAVIGATION SYSTEM (FANS) |
ICAS2012-10.1.3 |
| Mooij, M. |
A CAPABILITY FRAMEWORK FOR
MULTIPLE HETEROGENEOUS UAVS: FROM A MISSION COMMANDER'S PERSPECTIVE |
ICAS2012-9.7.3 |
| Moolchandani, K. A. |
DEVELOPING OPTIMAL AIRLINE
FLEETS UNDER ENVIRONMENTAL AND CAPACITY CONSTRAINTS |
ICAS2012-7.10.1 |
| Moormann, D. |
MODEL VALIDATION OF A
TILTWING UAV IN TRANSITION PHASE APPLYING WINDTUNNEL INVESTIGATIONS |
ICAS2012-11.1.1 |
| Moormann, D. |
CONTROL CONCEPT OF A
TILTWING UAV DURING LOW SPEED MANOEUVRING |
ICAS2012-11.1.2 |
| Moosavi, M. R. |
FINDING TUNING FREQUENCY OF
SYMMETRIC AND ANTI-SYMMETRIC LAMB WAVES USING FEM |
ICAS2012-P3.6 |
| Moreau, D. J. |
EXPERIMENTAL INVESTIGATION
OF FLAT PLATE SELF-NOISE REDUCTION USING TRAILING EDGE SERRATIONS |
ICAS2012-9.11.1 |
| Moreau, S. |
MULTI-OBJECTIVE OPTIMIZATION
OF MULTI-ELEMENT HIGH-LIFT AIRFOIL |
ICAS2012-2.3.4 |
| Moreau, S. |
TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS2012-4.4.4 |
| Moretti, G. |
PRELIMINARY INVESTIGATION ON
THE FEASIBILITY OF A BIRD SURROGATE FOR FULL-SCALE BIRD IMPACT TEST |
ICAS2012-8.3.1 |
| Morgan, R. G. |
STUDY OF RADIATIVE HEAT
TRANSFER IN TITAN ATMOSPHERIC ENTRY |
ICAS2012-3.8.3 |
| Mori, R. |
AIRCRAFT TAXIING MODEL AT
CONGESTED AIRPORTS |
ICAS2012-10.9.1 |
| Morinière, F. D. |
ENERGY DISTRIBUTION IN GLARE
AND 2024-T3 ALUMINIUM DURING LOW-VELOCITY IMPACT |
ICAS2012-7.7.2 |
| Mosharov, V. E. |
EXPERIMENTAL AND NUMERICAL
INVESTIGATIONS OF LOCAL AERODYNAMICS OF CIVIL AIRCRAFT |
ICAS2012-2.9.4 |
| Moss, S. D. |
BI-AXIAL VIBRATION ENERGY
HARVESTING FOR USE ON AEROSPACE PLATFORMS |
ICAS2012-6.7.1 |
| Mouritz, A. P. |
DAMAGE TOLERANCE OF Z-PINNED
COMPOSITE JOINTS |
ICAS2012-7.5.2 |
| Mouritz, A. P. |
DELAMINATION TOUGHENING OF
CARBON-EPOXY LAMINATE WITH A POLYETHYLENE-CO-METHACRYLIC ACID (EMAA)
SELF-HEALING MODIFIER |
ICAS2012-7.6.2 |
| Mouser, C. R. |
VIBRATION AND AEROELASTIC CLEARANCE WORK FOR JASSM INTEGRATION ONTO THE F/A-18A/B |
ICAS2012-8.10.3 |
| Mozzillo, R. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
| Mugrauer, R. |
ARTIFICIAL HINGED-WING
BIRD WITH ACTIVE TORSION AND PARTIALLY
LINEAR KINEMATICS |
ICAS2012-3.6.1 |
| Muhammad, H. |
DEVELOPMENT OF POSE
ESTIMATION SYSTEM BASED ON DUAL CAMERA TECHNIQUES FOR PARAMETER
IDENTIFICATION OF INDOOR MAV |
ICAS2012-11.9.4 |
| Mulyanto, T. |
DEVELOPMENT OF POSE
ESTIMATION SYSTEM BASED ON DUAL CAMERA TECHNIQUES FOR PARAMETER
IDENTIFICATION OF INDOOR MAV |
ICAS2012-11.9.4 |
| Mumaw, R. |
UNRELIABLE AIRSPEED – MAKING
VALID ASSUMPTIONS ON FLIGHT CREW PERFORMANCE |
ICAS2012-9.3.4 |
| Mundt, C. |
IMPROVED MODELLING OF
VORTICAL MIXING FOR THE SIMULATION OF EFFICIENT PROPULSION SYSTEMS |
ICAS2012-4.10.1 |
| Munoz, C. |
CONCEPT OF INTEGRATION FOR
UAS OPERATIONS IN THE NAS |
ICAS2012-10.7.1 |
| Murakami, K. |
AUTOMATIC HANDLING OF
DEFECTIVE SURFACE GEOMETRY WITHIN GRID GENERATION FOR NAVIER-STOKES
COMPUTATION |
ICAS2012-2.11.1 |
| Murakami, K. |
DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11.ST |
| Muraoka, K. |
TRANSITION FLIGHT OF QUAD
TILT WING VTOL UAV |
ICAS2012-11.1.3 |
| Muraoka, K. |
EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS2012-9.3.1 |
| Murayama, M. |
COMPUTATIONAL STUDY ON NOISE
GENERATION FROM A TWO-WHEEL MAIN LANDING GEAR |
ICAS2012-3.9.3 |
| Murozono, M. |
INVESTIGATION ON STRUCTURAL
AND AERODYNAMIC CHARACTERISTICS OF RESONANT TYPE ELASTIC FLAPPING WING |
ICAS2012-9.5.3 |
| Murphy, M. |
ICAO’S BALANCED APPROACH TO
NOISE MANAGEMENT AND ITS INFLUENCE ON THE ECONOMIC IMPACT OF AIR
TRANSPORTATION |
ICAS2012-7.10.4 |
| Muscat, A. |
A PROPOSAL FOR REVISED
APPROACHES AND PROCEDURES TO MALTA INTERNATIONAL AIRPORT |
ICAS2012-4.9.3 |
| Nagai, H. |
INVESTIGATION ON STRUCTURAL
AND AERODYNAMIC CHARACTERISTICS OF RESONANT TYPE ELASTIC FLAPPING WING |
ICAS2012-9.5.3 |
| Nagarathinam, A. |
ARTIFICIAL HINGED-WING
BIRD WITH ACTIVE TORSION AND PARTIALLY
LINEAR KINEMATICS |
ICAS2012-3.6.1 |
| Nagel, B. |
A KNOWLEDGE BASED APPROACH
FOR EXTENDED PHYSICS-BASED WING MASS ESTIMATION IN EARLY DESIGN STAGES |
ICAS2012-1.1.1 |
| Nagel, B. |
COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS2012-1.9.1 |
| Naghipour, P. |
NUMERICAL SIMULATIONS AND
EXPERIMENTAL INVESTIGATIONS ON QUASI-STATIC AND CYCLIC MIXED MODE
DELAMINATION OF MULTIDIRECTIONAL CFRP LAMINATES |
ICAS2012-7.4.2 |
| Nagy, A. |
MEASURING AND MODELLING THE
LONGITUDINAL MOTION OF PARAGLIDERS |
ICAS2012-5.10.2 |
| Nagy, A. |
UNMANNED MEASUREMENT
PLATFORM FOR PARAGLIDERS |
ICAS2012-P1.4 |
| Nakamura, H. |
SCIENCE AND TECHNOLOGY MAP
ANALYSIS OF AEROSPACE ENGINEERING |
ICAS2012-P7.1 |
| Nakamura, T. |
DEVELOPMENT OF LAPTOP PC
TOOL WITH VISUAL PROJECTION FOR FLIGHT MANAGEMENT TRAINING |
ICAS2012-9.10.ST |
| Nakamura, Y. |
FUNDAMENTAL CHARACTERISTICS
OF DECENTRALIZED AIR TRAFFIC FLOW CONTROL IN HIGH DENSITY CORRIDOR |
ICAS2012-10.7.2 |
| Nakata, N. |
MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1.ST2 |
| Nakatsuka, S. |
TITANIUM METAL MATRIX
COMPOSITE DEVELOPMENT FOR COMMERCIAL AIRCRAFT LANDING GEAR STRUCTURE |
ICAS2012-7.5.1 |
| Nam, H. J. |
MODELING OF NO AND OH
INFRARED RADIATION ON A CONVERGENT-DIVERGENT NOZZLE |
ICAS2012-P4.6 |
| Naruoka, M. |
REAL-TIME WAVELET FLIGHT
DATA EVALUATOR FOR SYSTEM IDENTIFICATION OF FLIGHT CHARACTERISTICS |
ICAS2012-5.10.4 |
| Naruoka, M. |
FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS2012-5.2.1 |
| Nayko, Y. |
AEROELASTIC
MULTIDISCIPLINARY ANALYSIS OF THE FIN
WITH INNOVATIVE ADAPTIVE CONTROL |
ICAS2012-8.7.4 |
| Neely, A. J. |
PROGRESS IN UNDERSTANDING
TRANSONIC AND SUPERSONIC GROUND EFFECT AERODYNAMICS |
ICAS2012-10.6.3 |
| Negishi, E. |
EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS2012-9.3.1 |
| Neilson, S. V. |
INVESTIGATION INTO OPTIMISED
COMPOSITE SCARF REPAIRS WITH PRACTICAL CONSTRAINTS |
ICAS2012-P3.4 |
| Nepomnyashchiy, A. D. |
THE EXPERIENCE OF HIGH
PRESSURE RATIO SINGLE STAGE HPT DESIGNING |
ICAS2012-P4.15 |
| Neuheuser, T. |
SYSTEM ANALYSIS OF
PROGNOSTICS AND HEALTH MANAGEMENT SYSTEMS FOR FUTURE TRANSPORT AIRCRAFT |
ICAS2012-12.3.1 |
| Neyland, V. Y. |
AN EXPERIENCE OF USING
NUMERICAL METHODS IN EXPERIMENTAL INVESTIGATIONS OF TsAGI |
ICAS2012-P2.6 |
| Ng, H. K. |
UNCERTAINTY QUANTIFICATION
IN THE DEVELOPMENT OF AVIATION OPERATIONS TO REDUCE AVIATION EMISSIONS AND
CONTRAILS |
ICAS2012-7.10.2 |
| Nguyen-Bui, N. T.-H. |
MODELING OF THE INTERACTION
BETWEEN A TURBULENT FLOW AND AN ABLATABLE MATERIAL |
ICAS2012-3.8.2 |
| Nguyen-Bui, T.-H. |
SIMULATION OF THE FULL
COUPLING BETWEEN THE RADIATION TRANSFER AND THE AERODYNAMICS FOR HYPERSONIC REENTRY PROBES |
ICAS2012-3.8.ST |
| Nicholson, K. J. |
A PLANAR ANTENNA ARRAY
MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC |
ICAS2012-6.11.ST |
| Nicholson, R. |
UNRELIABLE AIRSPEED – MAKING
VALID ASSUMPTIONS ON FLIGHT CREW PERFORMANCE |
ICAS2012-9.3.4 |
| Nicholson, R. K. |
CATEGORIZATION OF UNRELIABLE
AIRSPEED EVENTS USING RASMUSSEN’S HUMAN PERFORMANCE MODEL |
ICAS2012-9.4.4 |
| Nicke, E. |
STUDY ON NOISE OF COUNTER
ROTATING FAN MODELS AT CIAM ANECHOIC CHAMBER |
ICAS2012-3.9.4 |
| Nicolosi, F. |
AERODYNAMIC ANALYSIS AND
DESIGN OF A TWIN-ENGINE COMMUTER
AIRCRAFT |
ICAS2012-1.6.2 |
| Niedermeier, D. |
FLY-BY-WIRE AUGMENTED MANUAL
CONTROL - BASIC DESIGN CONSIDERATIONS |
ICAS2012-5.4.1 |
| Niehuis, R. |
NUMERICAL INVESTIGATION OF
THE EFFECT OF INFLOW DISTORTIONS ON TRANSONIC AXIAL COMPRESSOR STAGES WITH 2D
AND 3D CALCULATIONS |
ICAS2012-4.6.2 |
| Nieuwenhuisen, D. |
THE EREA VISION ON HIGH
PRIORITY RESEARCH AXES TOWARDS AIR TRANSPORT SYSTEM 2050 |
ICAS2012-1.7.1 |
| Nieuwenhuisen, D. |
OPTIMIZING INBOUND AIRCRAFT
STREAMS USING AIRCRAFT DERIVED DATA AND RTA FUNCTIONALITY |
ICAS2012-10.4.4 |
| Nigmatullin, R. Z. |
INTERDISCIPLINARY COMPLEX
DESIGN OF MODERN HIGH AND LOW PRESSURE TURBINES |
ICAS2012-4.3.3 |
| Ninomiya, T. |
GUIDANCE AND CONTROL LAW FOR
D-SEND#2 |
ICAS2012-5.3.1 |
| Nitsche, W. |
ACTIVE
SEPARATION CONTROL ON A 2D HIGH-LIFT WING SECTION TOWARDS HIGH REYNOLDS
NUMBER APPLICATION |
ICAS2012-3.5.3 |
| Nooij, S. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
| Noori, B. |
AN
APPROXIMATE ENGINEERING METHOD FOR AERODYNAMIC HEATING SOLUTION AROUND BLUNT
BODY NOES |
ICAS2012-11.4.4 |
| Nordin, P. |
AIRCRAFT SYSTEM SIMULATION
FOR PRELIMINARY DESIGN |
ICAS2012-1.9.3 |
| Nouri, Z. |
AN
OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES |
ICAS2012-6.5.ST |
| Nozhnitskiy, Y. A. |
VIBRATION STRENGTH INCREASE
OF ROTATING BLADES USING DYNAMIC SPIN RIGS |
ICAS2012-12.6.4 |
| Nozhnitskiy, Y. A. |
PREVENTION OF LOW CYCLE
FATIGUE FRACTURE OF AVIATION ENGINE CRITICAL PARTS |
ICAS2012-4.1.2 |
| Numata, D. |
MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1.ST2 |
| Nunes, N. |
ASSESSING
HELICOPTER SURVIVABILITY TO GROUND LAUNCHED PROJECTILES USING MULTI-FIDELITY
INVERSE SIMULATION |
ICAS2012-1.4.4 |
| Nurhakim, M. L. I. |
DEVELOPMENT OF POSE
ESTIMATION SYSTEM BASED ON DUAL CAMERA TECHNIQUES FOR PARAMETER
IDENTIFICATION OF INDOOR MAV |
ICAS2012-11.9.4 |
| O’Byrne, S. |
JET INTERACTION IN A
HYPERSONIC FLOW: A COMPARISON BETWEEN PLIF THERMOMETRY AND COMPUTATIONAL
SIMULATION |
ICAS2012-4.11.2 |
| Ogawa, H. |
ROBUST DESIGN OPTIMIZATION
OF HIGH-PERFORMANCE AXISYMMETRIC SCRAMJETS BASED ON SURROGATE-ASSISTED
EVOLUTIONARY ALGORITHMS |
ICAS2012-4.11.3 |
| Oh, H. -U. |
VERIFICATION OF OPTICAL
PAYLOAD CFRP STRUCTURE FOR SATELLITE THROUGH ANALYSIS AND SPACE QUALIFICATION
TEST |
ICAS2012-P3.9 |
| Ohira, K. |
NUMERICAL STUDY OF THE
REYNOLDS NUMBER EFFECT ON LOW ASPECT
RATIO WINGS AT LOW SPEED |
ICAS2012-2.10.2 |
| Ohira, K. |
DEVELOPMENT OF SUPERSONIC
NATURAL LAMINAR FLOW WING DESIGN SYSTEM USING CFD-BASED INVERSE METHOD |
ICAS2012-2.2.1 |
| Ohnuki, T. |
JAXA’S ENVIRONMENT CONSCIOUS
AIRCRAFT TECHNOLOGY PROGRAM PLAN |
ICAS2012-7.11.3 |
| Oh-Ohara, S. |
ESTIMATION OF AERODYNAMIC
DERIVATIVES IN AIRCRAFT MODEL USING ITERATIVE LEARNING IDENTIFICATION |
ICAS2012-5.10.5 |
| Ohsawa, R. |
DEVELOPMENT OF OBSERVATIONAL
SYSTEM WITH UNMANNED FLIGHT SYSTEM |
ICAS2012-P5.10 |
| Ohta, K. |
GUST RESPONSE ANALYSIS IN
THE FLIGHT FORMATION OF UNMANNED AIR VEHICLES |
ICAS2012-P5.9 |
| Okada, N. |
TRANSITION FLIGHT OF QUAD
TILT WING VTOL UAV |
ICAS2012-11.1.3 |
| Okumura, K. |
THE FLAPPING AIRCRAFT
DYNAMICS WITH WING DEFORMATION UNDER GUST INPUT |
ICAS2012-11.9.2 |
| Olbrechts, T. |
DESIGN STUDY OF AN ACTIVE
GURNEY FLAP SYSTEM FOR HELICOPTER ROTOR BLADES |
ICAS2012-6.11.1 |
| Olbrechts, T. |
IDENTIFICATION OF HELICOPTER
GROUND RESONANCE WITH MULTI-BODY SIMULATION |
ICAS2012-8.3.2 |
| Olbrechts, T. |
RELIABILITY ANALYSIS OF
AIRCRAFT SYSTEM ARCHITECTURES |
ICAS2012-P9.1 |
| Olsen, J. F. |
INFORMATION THEORY APPLIED
TO A SELF-ORGANISED, UNMANNED AERIAL SYSTEM |
ICAS2012-11.7.4 |
| Omer, J. |
AUTOMATED CONFLICT-FREE
PLANNING: EXPERIMENTS ON REAL AIR TRAFFIC DATA |
ICAS2012-10.1.2 |
| Onate, E. |
ROBUST AERODYNAMIC DESIGN
OPTIMISATION OF MORPHING AEROFOIL/WING USING DISTRIBUTED MOGA |
ICAS2012-11.10.3 |
| Ono, D. |
THEORETICAL AND EXPERIMENTAL
INVESTIGATIONS ON CHOKING PHENOMENA OF AXISYMMETRIC CONVERGENT NOZZLE FLOW |
ICAS2012-P2.11 |
| Orekhov, I. K. |
EXPERIMENTAL AND NUMERICAL
STUDY OF TWO FIRST HIGHLY-LOADED STAGES OF COMPRESSORS AS A PART OF HPC AND
SEPARATE UNIT |
ICAS2012-4.6.1 |
| Oreschko, B. |
DYNAMIC TURNAROUND
MANAGEMENT IN A HIGHLY AUTOMATED AIRPORT ENVIRONMENT |
ICAS2012-10.9.2 |
| Orifici, A. C. |
CRITICAL ASSESSMENT OF
FAILURE CRITERION FOR ADHESIVELY BONDED COMPOSITE JOINT REPAIR DESIGN |
ICAS2012-12.2.2 |
| Orifici, A. C. |
INVESTIGATION INTO OPTIMISED
COMPOSITE SCARF REPAIRS WITH PRACTICAL CONSTRAINTS |
ICAS2012-P3.4 |
| O'Shea, P. |
FIELD-OF-VIEW, DETECTION
RANGE, AND FALSE ALARM TRADE-OFFS IN VISION-BASED AIRCRAFT DETECTION |
ICAS2012-6.9.1 |
| Ostermann, T. |
MODEL VALIDATION OF A
TILTWING UAV IN TRANSITION PHASE APPLYING WINDTUNNEL INVESTIGATIONS |
ICAS2012-11.1.1 |
| Ostermann, T. |
CONTROL CONCEPT OF A
TILTWING UAV DURING LOW SPEED MANOEUVRING |
ICAS2012-11.1.2 |
| Oswald, J. J. |
EOLE, AN INNOVATIVE FLYING
SCALE DEMONSTRATOR FOR AIR-LAUNCH-TO-ORBIT AUTOMATIC SYSTEMS |
ICAS2012-1.11.2 |
| Öttl, G. |
A SCENARIO-BASED APPROACH TO
DEVELOP REPRESENTATIVE TRAFFIC ENVIRONMENTS FOR OPERATIONAL AIRCRAFT
EVALUATION |
ICAS2012-6.3.1 |
| Ozerciyes, V. |
TOOL DEVELOPMENT FOR
AIRCRAFT LOADS POST-PROCESSING |
ICAS2012-P3.5 |
| Paces, P. |
ADVANCED DISPLAY AND
POSITION ANGLES MEASUREMENT SYSTEMS |
ICAS2012-P6.3 |
| Pacino, M. |
VERY-LONG ENDURANCE SOLAR
POWERED AUTONOMOUS UAVS: ROLE AND CONSTRAINTS FOR GMES APPLICATIONS |
ICAS2012-4.7.5 |
| Page, J. |
ENGINE-OUT TAKEOFF PATH
OPTIMIZATION OUT OF TERRAIN CHALLENGING AIRPORTS |
ICAS2012-5.8.2 |
| Page, J. R. |
INFORMATION THEORY APPLIED
TO A SELF-ORGANISED, UNMANNED AERIAL SYSTEM |
ICAS2012-11.7.4 |
| Palizvan, M. |
POST-BUCKLING
BEHAVIOR AND PROPAGATION OF DELAMINATION FOR COMPOSITE PANELS IN DIFFERENT
DELAMINATION SIZES |
ICAS2012-7.9.ST |
| Palizvan, M. |
BUCKLING
AND POST-BUCKLING RESPONSES OF SQUARE LAMINATE WITH VARIOUS SHAPED CUTOUTS
UNDER DIFFERENT LOADINGS |
ICAS2012-P3.7 |
| Palmer, J. L. |
HARDWARE-IN-THE-LOOP
SIMULATION OF FUEL-CELL-BASED HYBRID-ELECTRICAL UAV PROPULSION |
ICAS2012-4.5.2 |
| Palmer, J. L. |
DEVELOPMENT OF A
HYBRID-ELECTRIC POWER-SYSTEM MODEL FOR A SMALL SURVEILLANCE AIRCRAFT |
ICAS2012-P6.4 |
| Paluch, P. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
| Pan, W. |
PATH PLANNING FOR MULTI
HELICOPTER COORDINATED RESCUE |
ICAS2012-P8.5 |
| Pankov, A. V. |
FATIGUE DESIGN PROCEDURE OF
LONGITUDINAL AND TRANSVERSE FUSELAGE JOINTS |
ICAS2012-12.4.2 |
| Paquet, J. B. |
AEROELASTIC SIMULATION OF
FLEXIBLE FLAPPING WING BASED ON STRUCTURAL FEM AND QUASI-STEADY AERODYNAMIC
MODEL |
ICAS2012-8.5.1 |
| Park, J. -W. |
A PEG-BASED ASCENDING
GUIDANCE ALGORITHM FOR RAMJET-POWERED VEHICLES |
ICAS2012-5.7.4 |
| Park, J. -W. |
UAV COLLISION AVOIDANCE VIA
OPTIMAL TRAJECTORY GENERATION METHOD |
ICAS2012-P5.5 |
| Parker, R. |
HOT END TECHNOLOGY FOR
ADVANCED, LOW EMISSION LARGE CIVIL AIRCRAFT ENGINES |
ICAS2012-4.10.2 |
| Patek, Z. |
WIND TUNNEL AND CFD STUDY OF
AIRFOIL WITH AIRBRAKE |
ICAS2012-10.6.ST1 |
| Patel, S. |
BOUNDARY LAYER TRANSITION
DETECTION USING TEMPERATURE SENSITIVE PAINT IN THE ARA TRANSONIC WIND TUNNEL |
ICAS2012-3.4.2 |
| Paton, R. |
INTERFACE DIFFUSION AND
MORPHOLOGY OF AEROSPACE GRADE EPOXY CO-CURED WITH THERMOPLASTIC POLYMERS |
ICAS2012-7.8.2 |
| Paull, A. |
HIFIRE: AN INTERNATIONAL COLLABORATION TO ADVANCE THE SCIENCE AND TECHNOLOGY OF HYPERSONIC FLIGHT |
ICAS2012-0.8 |
| Pavlenko, A. A. |
THE INVESTIGATION OF A
POSSIBILITY OF INCREASING THE LIFT-TO-DRAG RATIO OF A MANEUVERABLE AIRCRAFT
AT SUBSONIC SPEEDS |
ICAS2012-2.10.3 |
| Pearce, G. |
A FEASIBILITY STUDY FOR
MULTI-MATERIAL RETROFITTABLE ENERGY ABSORBING STRUCTURE FOR AGED HELICOPTER
SUBFLOOR |
ICAS2012-12.3.3 |
| Pearce, G. |
DIRECTIONAL ENHANCEMENT OF
COMPOSITE STRUCTURES ENERGY ABSORPTION USING MAGNETORHEOLOGICAL FLUIDS |
ICAS2012-7.8.1 |
| Pearce, G. |
EXPERIMENTAL DEVELOPMENT AND
ANALYSIS OF AN ACTIVE CRUSHING ELEMENT USING PRESSURIZED COMPOSITE TUBES |
ICAS2012-8.1.ST |
| Pearce, G. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
| Pechloff, A. |
SMALL DISTURBANCE
NAVIER-STOKES INVESTIGATIONS OF FIGHTER-TYPE-DELTA-WING PITCHING OSCILLATIONS |
ICAS2012-2.11.2 |
| Pëna, E. L. |
WEIGHT ON WHEEL SYSTEM BASED
ON STRAIN GAUGES |
ICAS2012-6.11.2 |
| Peng, X. B. |
STRUCTURAL
INTEGRITY ANALYSIS AND TEST OF FATIGUE CRITICAL LOCATION OF MA60 REGIONAL JET |
ICAS2012-7.9.4 |
| Perdones-Diaz, D. |
CFD BASED AEROELASTIC
CALCULATION OF PROPELLER LOADS |
ICAS2012-9.8.1 |
| Perez, T. |
COMPUTATIONAL ASPECTS OF
PROBABILISTIC ASSESSMENT OF UAS ROBUST AUTONOMY |
ICAS2012-9.2.2 |
| Perez, T. |
EVALUATION OF ROBUST
AUTONOMY AND IMPLICATIONS ON UAS DESIGN |
ICAS2012-9.4.2 |
| Periaux, J. |
ROBUST AERODYNAMIC DESIGN
OPTIMISATION OF MORPHING AEROFOIL/WING USING DISTRIBUTED MOGA |
ICAS2012-11.10.3 |
| Perner, M. |
IMPROVING THE PRODUCTION
QUALITY OF THE ADVANCED AUTOMATED FIBER PLACEMENT PROCESS BY MEANS OF ONLINE
PATH CORRECTION |
ICAS2012-6.1.3 |
| Persiani, F. |
DESIGN ANALYSIS FOR HYBRID
PROPULSION |
ICAS2012-6.7.5 |
| Persiani, F. |
INNOVATION IN MAN MACHINE
INTERFACES: USE OF 3D CONFORMAL SYMBOLS IN THE DESIGN OF FUTURE HUDS (HEAD UP
DISPLAYS) |
ICAS2012-9.7.2 |
| Persiani, F. |
A
META-HEURISTIC APPROACH TO SIMULATE TAXI OPERATIONS |
ICAS2012-P8.7 |
| Persson, I. |
EXTERNAL AERODYNAMIC
PRESSURE LOADS FOR A RIGID FIGHTER AIRCRAFT, A COMPARISON BETWEEN PSP AND CFD |
ICAS2012-10.6.2 |
| Persson, P. |
A COUPLED AERO AND
STRUCTURAL DYNAMICS MODEL FOR COMPUTATION OF UNSTEADY LOADS ON THE HELICOPTER
SKELDAR V200 |
ICAS2012-8.7.2 |
| Petersen, P. |
THE INFLUENCE OF TURBULENCE
INTENSITY ON THE FLOW STRUCTURE OVER A THIN AIRFOIL AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.2 |
| Petersson, O. |
MULTIDISCIPLINARY AIRFRAME
DESIGN OPTIMIZATION |
ICAS2012-0.4 |
| Petrov, A. V. |
AERODYNAMICS OF STOL
AIRPLANES WITH POWERED HIGH-LIFT SYSTEMS |
ICAS2012-9.5.2 |
| Pezzella, G. |
AEROTHERMODYNAMIC FIELD PAST
A REENTRY CAPSULE FOR SAMPLE RETURN MISSIONS |
ICAS2012-3.8.1 |
| Philippe, M. J. |
A PRACTICAL, ROUTE-BASED
APPROACH TO AIRSPACE CAPACITY MANAGEMENT |
ICAS2012-10.2.2 |
| Philit, M. |
DERIVATED TURBULENCE MODEL
TO PREDICT HARMONIC LOADS IN TRANSONIC SEPARATED FLOWS OVER A BUMP |
ICAS2012-4.6.4 |
| Picart, P. |
SUBSONIC WAKE FLOWS ANALYSIS
BY DIGITAL THREE-WAVELENGTHS HOLOGRAPHIC INTERFEROMETRY |
ICAS2012-3.11.3 |
| Pickhaver, T. W. |
A TECHNIQUE TO PREDICT THE
AERODYNAMIC LOSSES OF BATTLE DAMAGED WINGS |
ICAS2012-3.2.2 |
| Pingkarawat, K. |
DELAMINATION TOUGHENING OF
CARBON-EPOXY LAMINATE WITH A POLYETHYLENE-CO-METHACRYLIC ACID (EMAA)
SELF-HEALING MODIFIER |
ICAS2012-7.6.2 |
| Pinna, M. |
MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS2012-7.6.3 |
| Pinon, O. J. |
EVALUATING FLEXIBILITY IN
AIRPORT CAPACITY-ENHANCING TECHNOLOGY INVESTMENTS |
ICAS2012-P8.2 |
| Pisarev, V. S. |
INVESTIGATION OF CRACK
PROPAGATION BY OPTICAL INTERFEROMETRIC MEASUREMENTS OF LOCAL DEFORMATION
RESPONSE |
ICAS2012-7.9.2 |
| Pistek, A. |
ANALYTICAL METHOD FOR LIMIT
LOAD CAPACITY CALCULATION OF THIN WALLED AIRCRAFT STRUCTURES |
ICAS2012-8.2.ST |
| Pitt, S. |
SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS2012-7.2.2 |
| Plokhikh, V. P. |
ADVANCED AEROSPACE SYSTEMS
WITH INTERCONTINENTAL AND GLOBAL RANGE OF FLIGHT |
ICAS2012-1.5.2 |
| Plot, S. |
THE ONERA ELSA CFD SOFTWARE
: INPUT FROM RESEARCH AND FEEDBACK FROM INDUSTRY |
ICAS2012-2.1.1 |
| Plötner, K. |
MULTI-DISCIPLINARY DESIGN
AND FEASIBILITY STUDY OF DISTRIBUTED PROPULSION SYSTEMS |
ICAS2012-1.7.5 |
| Pogaru, S. |
A NON-WEIGHT BASED,
MANUFACTURING INFLUENCED DESIGN (MIND) METHODOLOGY FOR PRELIMINARY DESIGN |
ICAS2012-6.4.3 |
| Poirel, D. |
NUMERICAL SIMULATIONS OF
SELF-SUSTAINED AEROELASTIC OSCILLATIONS AT LOW REYNOLDS NUMBERS |
ICAS2012-2.6.3 |
| Polikarpov, V. G. |
METHODS AND FACILITIES TO BE
USED TO EVALUATE THE AIRCRAFT FLIGHT AND NAVIGATION EQUIPMENT IN FLIGHT TESTS |
ICAS2012-5.6.3 |
| Poovendran, R. |
BALANCING OPERATOR PRIVACY
AND FUTURE AIRSPACE SURVEILLANCE |
ICAS2012-P8.6 |
| Popelka, J. |
ADVANCED DISPLAY AND
POSITION ANGLES MEASUREMENT SYSTEMS |
ICAS2012-P6.3 |
| Porat, H. |
STUDY OF RADIATIVE HEAT
TRANSFER IN TITAN ATMOSPHERIC ENTRY |
ICAS2012-3.8.3 |
| Porretta, M. |
A COMPARISON OF
4D-TRAJECTORY OPERATIONS ENVISIONED FOR 'NEXTGEN' AND 'SESAR', SOME
PRELIMINARY FINDINGS |
ICAS2012-10.3.1 |
| Potekhina, I. |
EXPERIMENTAL AND NUMERICAL
RESEARCH OF UNSTEADY FLOW IN CURVILINEAR CHANNEL WITH ACTIVE FLOW MANAGEMENT
USING “SYNTHETIC” JETS |
ICAS2012-4.4.2 |
| Pradeepa, T. K. |
TRANSONIC FLUTTER, SHOCKS,
AND PARAMETER EFFECTS |
ICAS2012-2.6.4 |
| Premachandran, S. |
NUMERICAL STUDY ON THE
EFFECT OF VARYING SPANWISE TWIST ON LOW-REYNOLDS-NUMBER FLAPPING FLIGHT |
ICAS2012-2.5.1 |
| Prince, S. A. |
AN EXPERIMENTAL AND
NUMERICAL STUDY OF THE EFFECT OF NOSE BLUNTING ON A CONICAL NOSED BODY AT
TRANSONIC SPEED |
ICAS2012-2.8.3 |
| Prince, S. A. |
A COMPUTATIONAL STUDY OF THE
AERODYNAMICS OF A SPINNING CYLINDER IN CROSSFLOW OF HIGH REYNOLDS NUMBER |
ICAS2012-3.11.2 |
| Prince, S. A. |
AN EXPERIMENTAL STUDY OF A
PULSED AIR JET AND AN ACOUSTIC SYNTHETIC JET ON A LOW SPEED TURBULENT
BOUNDARY LAYER |
ICAS2012-3.5.1 |
| Prokofiev, A. B. |
THE INSTABILITY OF THE
PIPELINE DUE TO TRANSPORTING FLUID’S PRESSURE RIPPLES |
ICAS2012-8.11.1 |
| Prusty, B. G. |
DIRECTIONAL ENHANCEMENT OF
COMPOSITE STRUCTURES ENERGY ABSORPTION USING MAGNETORHEOLOGICAL FLUIDS |
ICAS2012-7.8.1 |
| Prusty, B. G. |
EXPERIMENTAL DEVELOPMENT AND
ANALYSIS OF AN ACTIVE CRUSHING ELEMENT USING PRESSURIZED COMPOSITE TUBES |
ICAS2012-8.1.ST |
| Prusty, G. |
A FEASIBILITY STUDY FOR
MULTI-MATERIAL RETROFITTABLE ENERGY ABSORBING STRUCTURE FOR AGED HELICOPTER
SUBFLOOR |
ICAS2012-12.3.3 |
| Prusty, G. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
| Pruter, I. |
FLIGHT PERFORMANCE OF
LIGHTWEIGHT GYROPLANES |
ICAS2012-5.6.2 |
| Qi, H. -F. |
THE FABRICATION AND
CHARACTERIZATION OF TiO2 UV DETECTOR |
ICAS2012-7.3.ST |
| Qi, H. T |
A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
| Qi, X. |
RESEARCH ON AIRBORNE
INTELLIGENT HYDRAULIC PUMP SYSTEM |
ICAS2012-6.10.3 |
| Qian, G. |
THE STUDY ON THE AIRCRAFT
INTEGRATED CHARACTERS WITH DIFFERENT HEIGHT WINGLETS |
ICAS2012-P2.9 |
| Qian, G. P. |
THE COMPREHENSIVE STUDY ON
ADVANCED WINGTIP DEVICES IN LARGE CIVIL AIRCRAFT |
ICAS2012-8.8.3 |
| Qian, R. Z. |
MULTI-OBJECTIVE AERODYNAMIC
OPTIMIZATION DESIGN OF MULTI-ELEMENT AIRFOIL USING KRIGING MODEL |
ICAS2012-2.3.ST |
| Qin, W. |
DEVELOPMENT
OF THE OPTIMIZED APPROACH AND LANDING TRAJECTORY FOR FUTURE AIR TRANSPORT
SYSTEM |
ICAS2012-P8.1 |
| Qu, T. |
ON
THE KNEE-POINT PHENOMENON IN COMPOSITE LAMINATES UNDER LOW-VELOCITY IMPACT
AND QUASI-STATIC INDENTATION |
ICAS2012-7.7.ST |
| Quaglia, D. |
TOWARDS TRAJECTORY
PREDICTION AND OPTIMISATION FOR ENERGY EFFICIENCY OF AN AIRCRAFT WITH
ELECTRICAL AND HYDRAULIC ACTUATION SYSTEMS |
ICAS2012-6.7.3 |
| Quagliotti, F. |
AN INNOVATIVE MISSION
MANAGEMENT SYSTEM FOR FIXED-WING UAVS |
ICAS2012-11.7.1 |
| Quagliotti, F. |
HYBRID GAME EVOLUTIONARY
ALGORITHM FOR MISSION PATH PLANNING OF AERIAL SURVEY TASKS |
ICAS2012-11.7.3 |
| Raabe, C. T. |
ADAPTIVE CONTROL INVERSION
AND ACTUATOR FAILURE COMPENSATION FOR UAVS |
ICAS2012-5.2.3 |
| Rad, T. |
DYNAMIC SEPARATION MINIMA
COUPLED WITH WAKE VORTEX PREDICTIONS IN DEPENDENT RUNWAY CONFIGURATIONS |
ICAS2012-10.4.2 |
| Radchenko, V. N. |
EXPERIMENTAL AND NUMERICAL
INVESTIGATIONS OF LOCAL AERODYNAMICS OF CIVIL AIRCRAFT |
ICAS2012-2.9.4 |
| Ragni, D. |
PROPELLER INDUCED GROUND
VORTEX |
ICAS2012-4.10.3 |
| Rajef, R. |
AN INVESTIGATION OF MODE I
FRACTURE TOUGHNESS USING ALIGNED CARBON-NANOTUBE FORESTS AT THE CRACK
INTERFACE |
ICAS2012-7.3.2 |
| Rajic, N. |
PROBING THE LIMITS - NEW
OPPORTUNITIES IN THERMOELASTIC STRESS ANALYSIS |
ICAS2012-12.1.1 |
| Rakotomamonjy, T. |
FAULT DETECTION AND
RECONFIGURATION APPLIED TO A HELICOPTER SWASHPLATE ACTUATOR |
ICAS2012-5.1.2 |
| Rambeau, C. |
TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS2012-4.4.4 |
| Rand, O. |
PERFORMANCE ANALYSIS OF A
COAXIAL ROTOR SYSTEM IN HOVER: THREE POINTS OF VIEW |
ICAS2012-2.7.4 |
| Rantet, E. |
EOLE, AN INNOVATIVE FLYING
SCALE DEMONSTRATOR FOR AIR-LAUNCH-TO-ORBIT AUTOMATIC SYSTEMS |
ICAS2012-1.11.2 |
| Rappa, G. |
HYBRID GAME EVOLUTIONARY
ALGORITHM FOR MISSION PATH PLANNING OF AERIAL SURVEY TASKS |
ICAS2012-11.7.3 |
| Raps, D. |
EVALUATION AND CORRELATION
OF INTER-LABORATORY RESULTS FROM A RAIN EROSION TEST CAMPAIGN |
ICAS2012-12.2.3 |
| Raps, D. |
COMPARATIVE EVALUATION OF
ICING ON AERODYNAMIC SURFACES |
ICAS2012-3.4.3 |
| Rasuo, B. |
MANEUVERABILITY OF AN UAV
WITH COANDA EFFECT BASED LIFT PRODUCTION |
ICAS2012-P2.18 |
| Ravi, S. |
THE INFLUENCE OF TURBULENCE
INTENSITY ON THE FLOW STRUCTURE OVER A THIN AIRFOIL AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.2 |
| Ravi, S. |
OPTIMUM LOCATION OF PRESSURE
MEASUREMENTS AROUND A WING AS A DYNAMIC CONTROL INPUT IN SMOOTH AND TURBULENT
CONDITIONS |
ICAS2012-3.3.3 |
| Ray, T. |
ROBUST DESIGN OPTIMIZATION
OF HIGH-PERFORMANCE AXISYMMETRIC SCRAMJETS BASED ON SURROGATE-ASSISTED
EVOLUTIONARY ALGORITHMS |
ICAS2012-4.11.3 |
| Razi, M. |
NONLINEAR AEROELASTIC
ANALYSIS OF SWEPT WINGS IN COMPRESSIBLE FLOW VIA THE HARMONIC BALANCE METHOD |
ICAS2012-8.7.1 |
| Razin, A. F. |
DEVELOPMENT OF GEODESIC
COMPOSITE AIRCRAFT STRUCTURES |
ICAS2012-8.4.2 |
| Reddy, R. |
NUMERICAL AND EXPERIMENTAL
ANALYSIS OF A REPRESENTATIVE ADF HELICOPTER FUSELAGE |
ICAS2012-2.7.2 |
| Renaud, G. |
PROBABILISTIC RISK ANALYSIS
FOR AIRCRAFT STRUCTURES WITH LIMITED IN-SERVICE DAMAGES |
ICAS2012-7.9.3 |
| Render, P. M. |
A TECHNIQUE TO PREDICT THE
AERODYNAMIC LOSSES OF BATTLE DAMAGED WINGS |
ICAS2012-3.2.2 |
| Ress, R. |
FLOW CHARACTERISTICS OF A
HELICOPTER FUSELAGE CONFIGURATION INCLUDING A ROTATING ROTOR HEAD |
ICAS2012-2.7.3 |
| Reu, T. K. |
CFD COMPUTATION OF THE
GROUND EFFECT ON AIRPLANE WITH HIGH ASPECT RATIO WING |
ICAS2012-P2.23 |
| Reymer, P. |
INTRODUCTION OF A STRUCTURE
INTEGRITY PROGRAM FOR A MILITARY TRAINER AIRCRAFT |
ICAS2012-12.6.2 |
| Rezaei, M. |
RISK ASSESSMENT MODELLING
FOR EVALUATING SAFETY AND IMPACT ON BUSINESS VIA A 3D RISK MATRIX |
ICAS2012-P9.2 |
| Ricci, S. |
NEOCASS: AN OPEN SOURCE
ENVIRONMENT FOR THE AEROELASTIC ANALYSIS AT CONCEPTUAL DESIGN LEVEL |
ICAS2012-8.10.1 |
| Riccobene, L. |
NEOCASS: AN OPEN SOURCE
ENVIRONMENT FOR THE AEROELASTIC ANALYSIS AT CONCEPTUAL DESIGN LEVEL |
ICAS2012-8.10.1 |
| Rieger, B. |
FLEXFOIL:
BIO-INSPIRED INTELLIGENT CONTROL ALGORITHM USING ARTIFICIAL NEURAL NETWORKS
FOR WING MORPHING |
ICAS2012-5.4.3 |
| Rinoie, K. |
STUDIES ON IMPROVEMENT OF
NONLINEAR PITCHING MOMENT CHARACTERISTICS OF CRANKED-ARROW WING |
ICAS2012-3.2.1 |
| Rinoie, K. |
DEVELOPMENT OF LAPTOP PC
TOOL WITH VISUAL PROJECTION FOR FLIGHT MANAGEMENT TRAINING |
ICAS2012-9.10.ST |
| Rizzi, A. |
COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS2012-1.9.1 |
| Roberts, G. |
TETHERING
UNMANNED ROTORCRAFT FOR HIGH-ENDURANCE OPERATIONS |
ICAS2012-P1.3 |
| Robertson, M. |
EFFECT ON THE AERODYNAMIC
FORCING IN AN AXIAL TURBINE STAGE ON VARYING STATOR BLADE SHAPE |
ICAS2012-4.3.ST |
| Rodde, A. -M. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
| Rodzewicz, M. |
DESIGN AND CONFIGURATION
LAYOUTS OF AN ADVANCED LONG ENDURANCE UAV- LESSONS LEARNT AFTER FLIGHT
TESTING |
ICAS2012-1.11.3 |
| Roestermundt, D. |
IMPROVING THE PRODUCTION
QUALITY OF THE ADVANCED AUTOMATED FIBER PLACEMENT PROCESS BY MEANS OF ONLINE
PATH CORRECTION |
ICAS2012-6.1.3 |
| Rogozin, V. V. |
FLIGHT TESTS OF TRANSPORT
AIRCRAFT UPSET RECOVERY TECHNIQUES AND THE SYSTEM OF INFORMATION SUPPORT OF
CREW |
ICAS2012-5.1.1 |
| Rohacs, D. |
RIDE CONTROL FOR THE
PERSONAL PLANE |
ICAS2012-5.3.2 |
| Rohacs, J. |
MEASURING AND MODELLING THE
LONGITUDINAL MOTION OF PARAGLIDERS |
ICAS2012-5.10.2 |
| Rohacs, J. |
RIDE CONTROL FOR THE
PERSONAL PLANE |
ICAS2012-5.3.2 |
| Rohacs, J. |
UNMANNED MEASUREMENT
PLATFORM FOR PARAGLIDERS |
ICAS2012-P1.4 |
| Romanelli, G. |
DESIGN AND VERIFICATION OF
FLUTTER SUPPRESSION CONTROL SYSTEMS BY MULTIDISCIPLINARY CO-SIMULATIONS |
ICAS2012-8.7.3 |
| Romeo, G. |
PRELIMINARY DESIGN OF A
FUEL-CELL-BASED HYBRID-ELECTRICAL UAV |
ICAS2012-1.8.2 |
| Romeo, G. |
VERY-LONG ENDURANCE SOLAR
POWERED AUTONOMOUS UAVS: ROLE AND CONSTRAINTS FOR GMES APPLICATIONS |
ICAS2012-4.7.5 |
| Romeo, G. |
MORE/ALL ELECTRIC AIRCRAFT
BASED ON FUEL CELL ENERGY SYSTEM: THE ENFICA-FC EXPERIENCE |
ICAS2012-6.7.2 |
| Rona, A. |
STREAMWISE AND CROSSFLOW
INSTABILITIES ON INCLINED CIRCULAR CYLINDERS |
ICAS2012-3.10.2 |
| Ronzheimer, A. |
A FULLY AUTOMATED CAD-BASED
FRAMEWORK FOR SHAPE OPTIMIZATION |
ICAS2012-11.10.1 |
| Rowlands, D. |
PROBING THE LIMITS - NEW
OPPORTUNITIES IN THERMOELASTIC STRESS ANALYSIS |
ICAS2012-12.1.1 |
| Rudenko, S. V. |
THE EXPERIENCE OF HIGH
PRESSURE RATIO SINGLE STAGE HPT DESIGNING |
ICAS2012-P4.15 |
| Ruiz-Calavera, L. P. |
CFD BASED AEROELASTIC
CALCULATION OF PROPELLER LOADS |
ICAS2012-9.8.1 |
| Ryabov, P. A. |
STUDIES
OF PROPULSION SYSTEM CONCEPTS FOR ADVANCED SUBSONIC AIRLINERS |
ICAS2012-4.7.3 |
| Rydell, S.A.H. |
A CASE STUDY OF ARRIVAL AND
DEPARTURE MANAGERS COOPERATION FOR REDUCING AIRBORNE HOLDING TIMES AT
DESTINATION AIRPORTS |
ICAS2012-10.1.ST |
| Rye, L. |
ALTERNATIVE AVIATION FUEL
FEEDSTOCK: THE MICROALGAE SOLUTION? |
ICAS2012-8.6.2 |
| Ryzhov, A. A. |
ENERGY SUPPLY EFFECT ON
SUPERSONIC BOUNDARY LAYER RECEPTIVITY AND STABILITY |
ICAS2012-P2.21 |
| Saad, M. R. |
EXPERIMENTAL STUDIES ON
MICRO-VORTEX GENERATORS IN HYPERSONIC FLOW |
ICAS2012-3.5.2 |
| Saad, M. R. |
PERFORMANCE ANALYSIS OF A
SCRAMJET INLET-ISOLATOR USING EXPERIMENTAL & NUMERICAL METHODS |
ICAS2012-P4.12 |
| Saarela, O. |
DIARC PLASMA COATING FOR
RELIABLE AND DURABLE STRUCTURAL BONDING OF METALS |
ICAS2012-7.2.1 |
| Sabatini, R. |
A CASE STUDY OF ARRIVAL AND
DEPARTURE MANAGERS COOPERATION FOR REDUCING AIRBORNE HOLDING TIMES AT
DESTINATION AIRPORTS |
ICAS2012-10.1.ST |
| Sabatini, R. |
TOWARDS TRAJECTORY
PREDICTION AND OPTIMISATION FOR ENERGY EFFICIENCY OF AN AIRCRAFT WITH
ELECTRICAL AND HYDRAULIC ACTUATION SYSTEMS |
ICAS2012-6.7.3 |
| Sabatini, R. |
CORRESPONDENCE AND
CLUSTERING METHODS FOR IMAGE-BASED WING-TIP COLLISION AVOIDANCE TECHNIQUES |
ICAS2012-9.10.4 |
| Sabatini, R. |
BI-OBJECTIVE PSEUDOSPECTRAL
OPTIMAL CONTROL TECHNIQUES FOR AIRCRAFT TRAJECTORY OPTIMIZATION |
ICAS2012-P5.6 |
| Saddoughi, S. |
THE EFFECT OF PLASMA
ACTUATORS ON TIP CLEARANCE FLOWS IN COMPRESSOR ROTORS |
ICAS2012-4.4.1 |
| Saegeler, S. |
IMPROVED MODELLING OF
VORTICAL MIXING FOR THE SIMULATION OF EFFICIENT PROPULSION SYSTEMS |
ICAS2012-4.10.1 |
| Sáez, F. J. |
HALA!: TOWARDS HIGHER LEVELS
OF AUTOMATION IN ATM. POSITION PAPER -STATE OF THE ART AND RESEARCH AGENDA |
ICAS2012-10.1.1 |
| Saha, A. |
ROBUST DESIGN OPTIMIZATION
OF HIGH-PERFORMANCE AXISYMMETRIC SCRAMJETS BASED ON SURROGATE-ASSISTED
EVOLUTIONARY ALGORITHMS |
ICAS2012-4.11.3 |
| Sahai, A. |
AN INTERDISCIPLINARY
APPROACH FOR A VIRTUAL AIR-TRAFFIC SYSTEM SIMULATION FOR SUBJECTIVE
ASSESSMENT IN VR ENVIRONMENTS |
ICAS2012-7.10.3 |
| Sahlman, S. |
DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS2012-10.4.1 |
| Sakashita, M. |
DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11.ST |
| Salam, I. R. |
METHODOLOGY FOR A
PRELIMINARY DESIGN STUDY OF A BOX-WING AIRLINER |
ICAS2012-1.10.3 |
| Salminen, E. |
SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS2012-10.6.1 |
| Sammut, A. |
RUNWAY CONFLICT ALERTING
DURING TAKE-OFF AND LANDING: ADVISORY OR DIRECTIVE? |
ICAS2012-9.10.1 |
| Sampigethaya, K. |
ENHANCING THE "LAST
MILE" COMMUNICATIONS AT AIRPORTS |
ICAS2012-10.10.5 |
| Sampigethaya, K. |
BALANCING OPERATOR PRIVACY
AND FUTURE AIRSPACE SURVEILLANCE |
ICAS2012-P8.6 |
| Sang, J. H. |
THE
INTEGRATION OPTIMIZATION DESIGN OF AERODYNAMIC AND STEALTH FOR FIGHTERS |
ICAS2012-P2.2 |
| Sang, J. H. |
EXPERIMENTAL
INVESTIGATION OF INFRARED STEALTH TECHNOLOGIES OF AERO-ENGINE EXHAUST SYSTEM |
ICAS2012-P4.1 |
| Santana, L. D. |
AIRFOIL SELF NOISE REDUCTION
BY APPLICATION OF DIFFERENT TYPES OF TRAILING EDGE SERRATIONS |
ICAS2012-3.11.1 |
| Sanz, L. P. |
AIRCRAFT FLIGHT TRAJECTORY
DEVIATION IN THE STANDARD INSTRUMENT DEPARTURES. OPERATORS PENALTIES |
ICAS2012-10.10.2 |
| Sarrat, C. |
MODELLING AIR TRAFFIC IMPACT
ON LOCAL AIR QUALITY WITH IESTA AND ADMS-AIRPORT: VALIDATION USING FIELD
MEASUREMENTS ON A REGIONAL AIRPORT |
ICAS2012-4.9.4 |
| Sarwe, P. |
MORE ELECTRICAL
ENVIRONMENTAL CONTROL SYSTEM SIMULATION |
ICAS2012-6.6.4 |
| Sato, M. |
TRANSITION FLIGHT OF QUAD
TILT WING VTOL UAV |
ICAS2012-11.1.3 |
| Sato, T. |
FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS2012-5.2.1 |
| Sato, T. |
TITANIUM METAL MATRIX
COMPOSITE DEVELOPMENT FOR COMMERCIAL AIRCRAFT LANDING GEAR STRUCTURE |
ICAS2012-7.5.1 |
| Sawa, T. |
ANALYTIC METHOD FOR FLIGHT
MOTION OF AIRCRAFT WITH A SINGLE VIDEO CAMERA AND ITS APPLICATION TO A FREE
FLIGHT GLIDER |
ICAS2012-5.6.1 |
| Schaefer, M. |
IMPACT OF ALTERNATIVE FUELS
ON ENGINE PERFORMANCE AND CO2-EMISSIONS |
ICAS2012-8.6.3 |
| Scharl, J. |
THE GENERALIZED ARRIVAL
PLANNER (GARP): MODELING AND ANALYSIS FOR ARRIVAL PLANNING |
ICAS2012-10.9.3 |
| Scharstein, F. |
ARTIFICIAL HINGED-WING
BIRD WITH ACTIVE TORSION AND PARTIALLY
LINEAR KINEMATICS |
ICAS2012-3.6.1 |
| Schiefele, J. |
OPERATIONAL
HUMAN-IN-THE-LOOP INTEGRATION OF 4D ARRIVAL GUIDANCE |
ICAS2012-5.8.1 |
| Schilling, T. |
SYSTEM ANALYSIS OF
PROGNOSTICS AND HEALTH MANAGEMENT SYSTEMS FOR FUTURE TRANSPORT AIRCRAFT |
ICAS2012-12.3.1 |
| Schmollgruber, P. |
AIRCRAFT CONCEPTUAL DESIGN
IN A MULTI-LEVEL, MULTI-FIDELITY, MULTI-DISCIPLINARY OPTIMIZATION PROCESS |
ICAS2012-1.6.4 |
| Schmollgruber, P. |
COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS2012-1.9.1 |
| Schofield, W. H. |
COLLABORATION CHALLENGES IN
THE GLOBAL AEROSPACE MARKET FOR SMALLER COUNTRIES - AN AUSTRALIAN PERSPECTIVE |
ICAS2012-0.1 |
| Scholtz, A. |
OPTIMIZATION OF A NEW
MULTI-PURPOSE UAS FOR SCIENTIFIC APPLICATIONS USING AERODYNAMIC
RECONFIGURATION |
ICAS2012-11.6.4 |
| Scholz, D. |
NOVEL LOW-FLYING
PROPELLER-DRIVEN AIRCRAFT CONCEPT FOR REDUCED DIRECT OPERATING COSTS AND
EMISSIONS |
ICAS2012-1.10.5 |
| Scholz, O. |
STEADY
AND UNSTEADY FLOWS PAST AIRFOILS AT LOW REYNOLDS NUMBERS IN THE PROXIMITY OF
THE GROUND |
ICAS2012-3.6.ST |
| Schönhals, S. |
DYNAMIC SEPARATION MINIMA
COUPLED WITH WAKE VORTEX PREDICTIONS IN DEPENDENT RUNWAY CONFIGURATIONS |
ICAS2012-10.4.2 |
| Schrempp, L. |
SHIELDING COSMIC RADIATION
IN AIR TRAFFIC |
ICAS2012-9.6.4 |
| Schuhmacher, G. |
MULTIDISCIPLINARY AIRFRAME
DESIGN OPTIMIZATION |
ICAS2012-0.4 |
| Schultz, M. |
DYNAMIC TURNAROUND
MANAGEMENT IN A HIGHLY AUTOMATED AIRPORT ENVIRONMENT |
ICAS2012-10.9.2 |
| Schumann, U. |
VOLCANIC, WEATHER AND
CLIMATE EFFECTS ON AIR TRANSPORT |
ICAS2012-0.6 |
| Schwob, C. |
MODELLING OF IMPACT ON
SANDWICH STRUCTURE FOR FAST MAINTENANCE LOOPS |
ICAS2012-8.3.3 |
| Seitz, A. |
MULTI-DISCIPLINARY DESIGN
AND FEASIBILITY STUDY OF DISTRIBUTED PROPULSION SYSTEMS |
ICAS2012-1.7.5 |
| Seitz, A. |
PROGRESS AND PERSPECTIVES OF
ELECTRIC AIR TRANSPORT |
ICAS2012-8.6.1 |
| Sekimoto, S. |
COMPUTATIONAL STUDY OF A
COMPARISON OF CO-FLOW AND COUNTER BLOWING DBD PLASMA ACTUATOR FOR SEPARATION
CONTROL OVER AN AIRFOIL |
ICAS2012-3.7.4 |
| Selivanov, O. D. |
STUDIES
OF PROPULSION SYSTEM CONCEPTS FOR ADVANCED SUBSONIC AIRLINERS |
ICAS2012-4.7.3 |
| Send, W. |
ARTIFICIAL HINGED-WING
BIRD WITH ACTIVE TORSION AND PARTIALLY
LINEAR KINEMATICS |
ICAS2012-3.6.1 |
| Senoguchi, A. |
DEVELOPMENT OF MOBILE
PASSIVE SECONDARY SURVEILLANCE RADAR |
ICAS2012-P8.8 |
| Seo, J. |
MULTIPLE UAV FORMATION
RECONFIGURATION WITH COLLISION AVOIDANCE GUIDANCE VIA DIFFERENTIAL GEOMETRY
CONCEPT |
ICAS2012-11.2.2 |
| Seong, K. |
HIDDEN MARKOV MODEL
PARAMETER ESTIMATION FOR MULTIPLE DIM TARGET DETECTION |
ICAS2012-P6.5 |
| Servetnik, A. N. |
ENERGY-BASED METHOD FOR GAS
TURBINE ENGINE DISK BURST SPEED CALCULATION |
ICAS2012-4.1.1 |
| Seth, K. |
DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS2012-10.4.1 |
| Seyfang, G. R. |
FANWING -- DEVELOPMENTS AND
APPLICATIONS |
ICAS2012-1.3.3 |
| Shadrin, D. V. |
VIBRATION STRENGTH INCREASE
OF ROTATING BLADES USING DYNAMIC SPIN RIGS |
ICAS2012-12.6.4 |
| Shakhmatov, E. V. |
THE INSTABILITY OF THE
PIPELINE DUE TO TRANSPORTING FLUID’S PRESSURE RIPPLES |
ICAS2012-8.11.1 |
| Shanmugam, J. |
PRODUCTION
OF BIO-FUEL FROM ALGAE BIOMASS, NANNOCHLOROPSIS OCULATA, FOR ADDITION TO
KEROSENE JET A-1 |
ICAS2012-8.6.4 |
| Shanygin, A. |
DESIGNING PRO-COMPOSITE
AIRCRAFT CONCEPTS AND LAYOUTS TO MAXIMIZE POTENTIAL BENEFITS OF HIGH SPECIFIC
STRENGTH OF CFRP |
ICAS2012-1.7.3 |
| Shanygin, A. N. |
STRENGTH CRITERIA
DEVELOPMENT FOR COMPOSITE STRUCTURES BASING ON SOLUTIONS SUPERPOSITION FOR
MODELS OF DIFFERENT LEVELS |
ICAS2012-7.1.2 |
| Sharifzadeh, S. |
DESIGN AND AERO-ELASTIC
OPTIMISATION OF THE STRUCTURE OF THE LAPCAT A2 MACH 5 AIRLINER |
ICAS2012-8.4.3 |
| Sharma, M. |
FLEXFOIL:
BIO-INSPIRED INTELLIGENT CONTROL ALGORITHM USING ARTIFICIAL NEURAL NETWORKS
FOR WING MORPHING |
ICAS2012-5.4.3 |
| Sharp, P. K. |
INITIAL RESULTS FROM DSTO’S
CORROSION STRUCTURAL INTEGRITY ROADMAP |
ICAS2012-12.6.1 |
| Shekhter, A. |
INITIAL RESULTS FROM DSTO’S
CORROSION STRUCTURAL INTEGRITY ROADMAP |
ICAS2012-12.6.1 |
| Shelley, A. E. |
PILOT CONVECTIVE WEATHER
DECISION MAKING IN EN ROUTE AIRSPACE |
ICAS2012-10.4.3 |
| Shen, Z. |
ON
THE KNEE-POINT PHENOMENON IN COMPOSITE LAMINATES UNDER LOW-VELOCITY IMPACT
AND QUASI-STATIC INDENTATION |
ICAS2012-7.7.ST |
| Sheynin, Y. |
A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS2012-6.11.3 |
| Shi, L. |
A GENERAL FOOTPRINT
GENERATION APPROACH FOR LIFTING RE-ENTRY VEHICLE |
ICAS2012-5.7.2 |
| Shim, S. -W. |
HIDDEN MARKOV MODEL
PARAMETER ESTIMATION FOR MULTIPLE DIM TARGET DETECTION |
ICAS2012-P6.5 |
| Shimagaki, M. |
INTEGRATED DESIGN METHOD OF
A ROCKET ENGINE TURBOPUMP SUB-SYSTEM FOR SUPPRESSING ROTOR LATERAL VIBRATION |
ICAS2012-4.3.4 |
| Shiomi, K. |
DEVELOPMENT AND EVALUATION
OF FATIGUE AND DROWSINESS PREDICTOR |
ICAS2012-9.6.1 |
| Shiomi, K. |
DEVELOPMENT OF MOBILE
PASSIVE SECONDARY SURVEILLANCE RADAR |
ICAS2012-P8.8 |
| Shiryaeva, A. A. |
APPLICATION OF THE FAST
CALCULATION TECHNOLOGIES TO SIMULATION OF NON-STATIONARY SUPERSONIC VISCID
FLOW WITH COMBUSTION |
ICAS2012-6.2.3 |
| Shmilovich, A. |
HIGH-LIFT SYSTEMS FOR
ENHANCED TAKEOFF PERFORMANCE |
ICAS2012-9.5.1 |
| Shoji, H. |
EVALUATION ON DISCRETE
SOURCE DAMAGES OF CFRP STIFFENED PANELS |
ICAS2012-7.7.1 |
| Shurman, V. |
A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS2012-6.11.3 |
| Shvirev, A. A. |
THE EXPERIENCE OF HIGH
PRESSURE RATIO SINGLE STAGE HPT DESIGNING |
ICAS2012-P4.15 |
| Si, J. |
THE STUDY ON THE AIRCRAFT
INTEGRATED CHARACTERS WITH DIFFERENT HEIGHT WINGLETS |
ICAS2012-P2.9 |
| Si, J. T. |
THE COMPREHENSIVE STUDY ON
ADVANCED WINGTIP DEVICES IN LARGE CIVIL AIRCRAFT |
ICAS2012-8.8.3 |
| Sibilski, K. |
A HIGHLY EXPANDABLE LOW-COST
OPEN-SOURCE UAV SYSTEM WITH HIGH ON-BOARD PROCESSING POWER |
ICAS2012-1.8.1 |
| Sichev, V. K. |
THE EXPERIENCE OF HIGH
PRESSURE RATIO SINGLE STAGE HPT DESIGNING |
ICAS2012-P4.15 |
| Siddens, A. J. |
DETAILED POST-SOFT IMPACT
PROGRESSIVE DAMAGE ANALYSIS FOR A HYBRID STRUCTURE JET ENGINE |
ICAS2012-4.2.3 |
| Siddens, A. J. |
COUPLED
MICROMECHANICS-FINITE ELEMENT PROGRESSIVE FAILURE DYNAMIC ANALYSIS APPROACH:
F-16 CANOPY CASE STUDY |
ICAS2012-7.7.5 |
| Sidoryuk, M. |
AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS2012-3.1.2 |
| Siikonen, T. |
SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS2012-10.6.1 |
| Silva, S. S. |
CATEGORIZATION OF UNRELIABLE
AIRSPEED EVENTS USING RASMUSSEN’S HUMAN PERFORMANCE MODEL |
ICAS2012-9.4.4 |
| Simkins, D. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
| Simon, P. |
IMPROVEMENTS FOR OPTIMUM
PROFILE SCHEDULING OF USER PREFERRED TRAJECTORIES |
ICAS2012-10.3.2 |
| Sizmann, A. |
PROGRESS AND PERSPECTIVES OF
ELECTRIC AIR TRANSPORT |
ICAS2012-8.6.1 |
| Sizmann, A. |
SHIELDING COSMIC RADIATION
IN AIR TRAFFIC |
ICAS2012-9.6.4 |
| Skomorokhov, S. I. |
AN EXPERIENCE IN AERODYNAMIC
DESIGN OF TRANSPORT AIRCRAFT |
ICAS2012-2.9.3 |
| Slobodkina, F. A. |
NUMERICAL MODELING OF FLOW
IN GASDYNAMIC RESONATOR AND MODEL VALIDATION BY RESULTS OF PULSE ENGINE TESTS |
ICAS2012-P4.10 |
| Smaili, H. |
AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS2012-3.1.2 |
| Smart, M. |
HIFIRE: AN INTERNATIONAL COLLABORATION TO ADVANCE THE SCIENCE AND TECHNOLOGY OF HYPERSONIC FLIGHT |
ICAS2012-0.8 |
| Smart, M. K. |
STREAMWISE PORTHOLE FUEL
INJECTION FOR BOUNDARY-LAYER COMBUSTION INSIDE A SCRAMJET ENGINE |
ICAS 2012-P4.16 |
| Smith, D. D. |
COMPUTATIONAL AND
EXPERIMENTAL ANALYSIS OF THE ACTIVE MORPHING WING CONCEPT |
ICAS2012-2.5.3 |
| Smrcek, L. |
ADVANCE SEAPLANE CONCEPTUAL
DESIGN ADAPTING TRIMARAN BOAT HULL CONCEPT |
ICAS2012-2.1.3 |
| Söderberg, R. |
ROBUST LIFECYCLE
OPTIMIZATION OF TURBINE COMPONENTS USING SIMULATION PLATFORMS |
ICAS2012-4.3.2 |
| Soemarwoto, B. |
AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS2012-3.1.2 |
| Sohier, H. |
EOLE, AN INNOVATIVE FLYING
SCALE DEMONSTRATOR FOR AIR-LAUNCH-TO-ORBIT AUTOMATIC SYSTEMS |
ICAS2012-1.11.2 |
| Solcia, T. |
DESIGN AND VERIFICATION OF
FLUTTER SUPPRESSION CONTROL SYSTEMS BY MULTIDISCIPLINARY CO-SIMULATIONS |
ICAS2012-8.7.3 |
| Soltani, Z. |
WAVELET-BASED ACTIVE SENSING
FOR QUANTITATIVE ASSESSMENT OF THROUGH-THICKNESS CRACK SIZE AND ANGLE IN
COMPOSITE PLATES |
ICAS2012-P3.8 |
| Song, B. |
AERODYNAMICS ANALYSIS OF
CYCLOIDAL ROTOR |
ICAS2012-2.7.1 |
| Song, B. F. |
NUMERICAL STUDY OF PITCHING
OSCILLATION EFFECT ON AERODYNAMIC CHARACTERISTICS OVER ASYMMETRIC VORTEX
STRUCTURE OF SLENDER REVOLUTION |
ICAS2012-2.5.2 |
| Song, J. |
FLOW CONTROL USING DBD
PLASMA ON BACKWARD-FACING STEP |
ICAS2012-3.7.3 |
| Song, J. |
THERMAL ANALYSIS NEAR
SECONDARY INJECTION HOLE IN SITVC SYSTEM |
ICAS2012-P4.9 |
| Song, W. -J. |
A NEW METHOD OF CALCULATION
THE DELAY TIME OF MULTI-CREW MEMBER EJECTION |
ICAS2012-P6.2 |
| Song, W. P. |
COMPARISON OF INFILL
SAMPLING CRITERIA IN KRIGING-BASED AERODYNAMIC OPTIMIZATION |
ICAS2012-11.10.ST |
| Song, W. P. |
LAMINAR FLOW WING’S
OPTIMIZATION DESIGN BY RANS SOLVER WITH AUTOMATIC TRANSITION PREDICTION |
ICAS2012-2.2.3 |
| Song, W. -P. |
DESIGN OF LAMINAR
SUPERCRITICAL AIRFOILS BASED ON NAVIER-STOKES EQUATIONS |
ICAS2012-2.2.2 |
| Sosebee, P. D. |
WATER TUNNEL FORCE AND
MOMENT STUDIES OF A MANEUVERING UCAV 1303 AND THEIR CONTROL |
ICAS2012-3.1.3 |
| Soudakov, V. G. |
EXPERIMENTAL AND NUMERICAL
INVESTIGATIONS OF LOCAL AERODYNAMICS OF CIVIL AIRCRAFT |
ICAS2012-2.9.4 |
| Soudakov, V. G. |
ENERGY SUPPLY EFFECT ON
SUPERSONIC BOUNDARY LAYER RECEPTIVITY AND STABILITY |
ICAS2012-P2.21 |
| Soulat, L. |
MULTI-OBJECTIVE OPTIMIZATION
OF MULTI-ELEMENT HIGH-LIFT AIRFOIL |
ICAS2012-2.3.4 |
| Soulat, L. |
TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS2012-4.4.4 |
| Sridhar, B. |
UNCERTAINTY QUANTIFICATION
IN THE DEVELOPMENT OF AVIATION OPERATIONS TO REDUCE AVIATION EMISSIONS AND
CONTRAILS |
ICAS2012-7.10.2 |
| Staack, I. |
PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS2012-1.6.1 |
| Staack, I. |
MORE ELECTRICAL
ENVIRONMENTAL CONTROL SYSTEM SIMULATION |
ICAS2012-6.6.4 |
| Stalewski, W. |
OPTIMISATION OF THE
HELICOPTER FUSELAGE WITH SIMULATION OF MAIN AND TAIL ROTOR INFLUENCE |
ICAS2012-1.4.1 |
| Stanfield, S. |
HIFIRE-1 BOUNDARY-LAYER
TRANSITION MEASUREMENTS |
ICAS2012-3.10.3 |
| Stanisak, M. |
GBAS CURVED APPROACH
PROCEDURES: ADVANTAGES, CHALLENGES AND APPLICABILITY |
ICAS2012-4.9.2 |
| Stanley, D. S. |
NON-LINEAR BEHAVIOUR OF A
WING DUE TO UNDERWING STORES |
ICAS2012-10.6.ST2 |
| Steen, M. |
GBAS CURVED APPROACH
PROCEDURES: ADVANTAGES, CHALLENGES AND APPLICABILITY |
ICAS2012-4.9.2 |
| Stefaniak, D. |
SEMI-ANALYTICAL SPRING-IN
ANALYSIS TO COUNTERACT CFRP MANUFACTURING DEFORMATIONS BY TOOL COMPENSATION |
ICAS2012-8.2.2 |
| Steiner, H.-J. |
MULTI-DISCIPLINARY DESIGN
AND FEASIBILITY STUDY OF DISTRIBUTED PROPULSION SYSTEMS |
ICAS2012-1.7.5 |
| Stephani, P. |
SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS2012-10.6.1 |
| Stepniczka, I. |
HMIAC – SURVEY ON
HUMAN-MACHINE INTERACTION IN AIRCRAFT COCKPITS |
ICAS2012-9.7.4 |
| Stokes, N. |
EXTERNAL AERODYNAMIC
PRESSURE LOADS FOR A RIGID FIGHTER AIRCRAFT, A COMPARISON BETWEEN PSP AND CFD |
ICAS2012-10.6.2 |
| Stokes, N. |
BOUNDARY LAYER TRANSITION
DETECTION USING TEMPERATURE SENSITIVE PAINT IN THE ARA TRANSONIC WIND TUNNEL |
ICAS2012-3.4.2 |
| Storm, T. M. |
BEYOND TWO-EQUATION
TURBULENCE MODELING FOR THE REYNOLDS-AVERAGED NAVIER-STOKES EQUATIONS:
ADVANCES IN COMPLEX FLOW PREDICTIONS |
ICAS2012-2.4.1 |
| Strobl, T. |
COMPARATIVE EVALUATION OF
ICING ON AERODYNAMIC SURFACES |
ICAS2012-3.4.3 |
| Stroehlein, T. |
DESIGN, DEVELOPMENT AND
MANUFACTURING OF THE ALCAS CFRP DOOR SURROUND STRUCTURE |
ICAS2012-8.8.1 |
| Stückl, S. |
VOLTAIR - THE ALL ELECTRIC
PROPULSION CONCEPT PLATFORM – A VISION FOR ATMOSPHERIC FRIENDLY FLIGHT |
ICAS2012-4.7.2 |
| Stumpf, E. |
MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS2012-6.4.1 |
| Stumpf, E. |
AN INTERDISCIPLINARY
APPROACH FOR A VIRTUAL AIR-TRAFFIC SYSTEM SIMULATION FOR SUBJECTIVE
ASSESSMENT IN VR ENVIRONMENTS |
ICAS2012-7.10.3 |
| Su, B. |
CRACK NUCLEATION MODELING IN
NOTCHED SPECIMEN SUBJECTED TO HIGH FATIGUE LOADING |
ICAS2012-7.7.4 |
| Subbaramaiah, R. |
A FEASIBILITY STUDY FOR
MULTI-MATERIAL RETROFITTABLE ENERGY ABSORBING STRUCTURE FOR AGED HELICOPTER
SUBFLOOR |
ICAS2012-12.3.3 |
| Sugimoto, S. |
EVALUATION ON DISCRETE
SOURCE DAMAGES OF CFRP STIFFENED PANELS |
ICAS2012-7.7.1 |
| Sun, F. -L. |
THE FABRICATION AND
CHARACTERIZATION OF TiO2 UV DETECTOR |
ICAS2012-7.3.ST |
| Sun, J. N. |
STUDY OF THE PRESSURE DROP
FOR RADIAL INFLOW BETWEEN CO-ROTATING DISCS |
ICAS2012-4.4.ST |
| Sun, J. Y. |
INVESTIGATION OF AIRBORNE
PRODUCT EXPENDING DYNAMIC CALIBRATION LIFE METHODS |
ICAS2012-12.5.2 |
| Sun, S. |
MICROSTRUCTURE AND
MECHANICAL PROPERTIES OF LASER CLADDING REPAIR OF AISI 4340 STEEL |
ICAS2012-12.4.4 |
| Sun, X. |
TECHNOLOGY ASSESSMENT OF
FUTURE AIRCRAFT: SOCIO-ECO-EFFICIENCY IN CONCEPTUAL AIRCRAFT DESIGN |
ICAS2012-1.9.2 |
| Sun, X. |
MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS2012-6.4.1 |
| Sun, Y. -F. |
A PRELIMINARY CFD
INVESTIGATION ON REAR FUSELAGE SUPPORT CORRECTION |
ICAS2012-P2.14 |
| Sundaresan, C. |
A METHODOLOGY FOR PARAMETRIC
PRODUCTION PLANNING IN PRELIMINARY AIRCRAFT DESIGN |
ICAS2012-6.4.4 |
| Surini, A. |
EXPERIMENTAL AND NUMERICAL
ASSESSMENT OF HELICOPTER SUBFLOOR CRASHWORTHINESS |
ICAS2012-8.1.1 |
| Suvorova, E. |
A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS2012-6.11.3 |
| Suzuki, A. |
DEVELOPMENT AND EVALUATION
OF FATIGUE AND DROWSINESS PREDICTOR |
ICAS2012-9.6.1 |
| Suzuki, H. |
GUIDANCE AND CONTROL LAW FOR
D-SEND#2 |
ICAS2012-5.3.1 |
| Suzuki, S. |
HIGH ANGLE OF ATTACK FLIGHT
CONTROL OF A TAIL-SITTER UNMANNED AIRCRAFT |
ICAS2012-11.8.2 |
| Suzuki, S. |
FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS2012-5.2.1 |
| Suzuki, S. |
INSIDE THE PILOTS MIND:
VISUAL INFORMATION USE IN MANUAL AIRCRAFT LANDINGS |
ICAS2012-9.7.1 |
| Suzuki, S. |
SCIENCE AND TECHNOLOGY MAP
ANALYSIS OF AEROSPACE ENGINEERING |
ICAS2012-P7.1 |
| Svirsky, Y. |
OUTLINE OF AIRCRAFT
STRUCTURE HEALTH AND USAGE MONITORING SYSTEMS AND METHODS USED FOR THEIR
REALIZATIONS |
ICAS2012-12.1.2 |
| Swieringa, K. |
INTERVAL MANAGEMENT WITH
SPACING TO PARALLEL DEPENDENT RUNWAYS (IMSPIDR) EXPERIMENT AND RESULTS |
ICAS2012-9.10.3 |
| Szolloz, A. |
GLOBAL OPTIMIZATION OF
TWO-DIMENSIONAL HIGH LIFT AERODYNAMIC SYSTEM |
ICAS2012-11.10.2 |
| Tahk, M. -J. |
CONTROLLER DESIGN AND
ANALYSIS OF UNMANNED AERIAL VEHICLES USING AUTOMATIC GAIN GENERATION
TECHNIQUE |
ICAS2012-11.8.1 |
| Tahk, M. -J. |
A PEG-BASED ASCENDING
GUIDANCE ALGORITHM FOR RAMJET-POWERED VEHICLES |
ICAS2012-5.7.4 |
| Tahk, M. -J. |
AUTOPILOT DESIGN FOR AN
AGILE MISSILE USING L1 ADAPTIVE BACKSTEPPING CONTROL |
ICAS2012-P5.4 |
| Tahk, M. -J. |
UAV COLLISION AVOIDANCE VIA
OPTIMAL TRAJECTORY GENERATION METHOD |
ICAS2012-P5.5 |
| Tahk, M. -J. |
TERRAIN REFERENCED UAV
NAVIGATION WITH LIDAR - A COMPARISON OF SEQUENTIAL PROCESSING AND BATCH
PROCESSING ALGORITHMS |
ICAS2012-P5.7 |
| Tahk, M. -J. |
HIDDEN MARKOV MODEL
PARAMETER ESTIMATION FOR MULTIPLE DIM TARGET DETECTION |
ICAS2012-P6.5 |
| Takahashi, N. |
TITANIUM METAL MATRIX
COMPOSITE DEVELOPMENT FOR COMMERCIAL AIRCRAFT LANDING GEAR STRUCTURE |
ICAS2012-7.5.1 |
| Takahashi, R. |
FORMATION SHAPE CONTROL OF
UNMANNED AIR VEHICLES |
ICAS2012-P5.8 |
| Takalani, L. S. |
A PRACTICAL, ROUTE-BASED
APPROACH TO AIRSPACE CAPACITY MANAGEMENT |
ICAS2012-10.2.2 |
| Takanobu, H. |
GUST RESPONSE ANALYSIS IN
THE FLIGHT FORMATION OF UNMANNED AIR VEHICLES |
ICAS2012-P5.9 |
| Takeda, S. |
EVALUATION ON DISCRETE
SOURCE DAMAGES OF CFRP STIFFENED PANELS |
ICAS2012-7.7.1 |
| Takeichi, N. |
FUNDAMENTAL CHARACTERISTICS
OF DECENTRALIZED AIR TRAFFIC FLOW CONTROL IN HIGH DENSITY CORRIDOR |
ICAS2012-10.7.2 |
| Takeichi, N. |
CONTINUOUS DESCENT
TRAJECTORY WITH OPTIMUM ARRIVAL TIME CONTROLLABILITY |
ICAS2012-P8.3 |
| Takovitskii, S. A. |
ELLIPTICALLY CONICAL TWIST
AND CAMBER OF DELTA WINGS |
ICAS2012-2.8.2 |
| Talbotec, J. |
STUDY ON NOISE OF COUNTER
ROTATING FAN MODELS AT CIAM ANECHOIC CHAMBER |
ICAS2012-3.9.4 |
| Tamagnone Cosmelli, F. |
MULTIDISCIPLINARY DESIGN AND
FLIGHT TESTING OF A REMOTE GAS/PARTICLE AIRBORNE SENSOR SYSTEM |
ICAS2012-6.10.4 |
| Tan, Z. |
RESEARCH FOR JET FLOW INFLUENCES TO WING-MOUNTED CIVIL
AIRCRAFT AERODYNAMIC CHARACTERISTICS |
ICAS2012-2.9.1 |
| Tanaka, N. |
VISUALIZATION OF UNSTEADY
BEHAVIOR OF SHOCK WAVES AROUND SUPERSONIC INTAKE INSTALLED IN SHOCK TUNNEL |
ICAS2012-P4.5 |
| Tanatsugu, N. |
DEVELOPMENT OF A SMALL-SCALE
SUPERSONIC FLIGHT EXPERIMENT VEHICLE AS A FLYING TEST BED |
ICAS2012-1.2.2 |
| Tang, J. |
AERODYNAMICS ANALYSIS OF
CYCLOIDAL ROTOR |
ICAS2012-2.7.1 |
| Tang, M. |
CHARACTERISTICS
OF AN 80-DEG SWEPT DELTA WING IN WING ROCK OR FREE YAWING |
ICAS2012-3.1.ST1 |
| Tang, M. Z. |
FLOW
CONTROL TEST RESEARCH OF AIRCRAFT MODEL WITH ADJUSTABLE CANAEDS |
ICAS2012-P2.5 |
| Tang, Z. |
A METHODOLOGY FOR PARAMETRIC
PRODUCTION PLANNING IN PRELIMINARY AIRCRAFT DESIGN |
ICAS2012-6.4.4 |
| Tani, Y. |
EXPERIMENTAL STUDY OF THE
MORPHING FLAP AS A LOW NOISE HIGH LIFT DEVICE FOR AIRCRAFT WING |
ICAS2012-9.11.3 |
| Tao, C. H. |
FRACTURE
ANALYSIS OF BLADE DOVETAIL OF TC11 TITANIUM ALLOY |
ICAS2012-P4.7 |
| Tarasov, A. I. |
NUMERICAL MODELING OF FLOW
IN GASDYNAMIC RESONATOR AND MODEL VALIDATION BY RESULTS OF PULSE ENGINE TESTS |
ICAS2012-P4.10 |
| Taylor, S. |
BALANCING OPERATOR PRIVACY
AND FUTURE AIRSPACE SURVEILLANCE |
ICAS2012-P8.6 |
| Techakesari, O. |
DESIGN OF FLIGHT AVOIDANCE
MANOEUVRE ALPHABETS FOR MIXED CENTRALISED-DECENTRALISED SEPARATION MANAGEMENT |
ICAS2012-10.7.3 |
| Teimouri, B. |
RISK ASSESSMENT MODELLING
FOR EVALUATING SAFETY AND IMPACT ON BUSINESS VIA A 3D RISK MATRIX |
ICAS2012-P9.2 |
| Tenno, T. |
DESIGN OF ROBUST FLIGHT
CONTROL SYSTEM FOR SMALL FIXED-WING UAV |
ICAS2012-11.9.3 |
| Tervakangas, S. |
DIARC PLASMA COATING FOR
RELIABLE AND DURABLE STRUCTURAL BONDING OF METALS |
ICAS2012-7.2.1 |
| Tetzloff, I. J. |
MEASURING SYSTEM-WIDE
IMPACTS OF NEW AIRCRAFT ON THE ENVIRONMENT |
ICAS2012-7.11.1 |
| Tezuka, A. |
DEVELOPMENT OF LAPTOP PC
TOOL WITH VISUAL PROJECTION FOR FLIGHT MANAGEMENT TRAINING |
ICAS2012-9.10.ST |
| Thielecke, F. |
MODEL BASED DESIGN AND
EXPERIMENTAL VALIDATION OF ELECTRO-MECHANIC ACTUATOR SYSTEMS FOR A NOSE
LANDING GEAR |
ICAS2012-6.8.3 |
| Thomas, P. J. |
ON THE EFFECT OF DISTRIBUTED
ROUGHNESS ON TRANSITION OVER ROTOR-STATOR DEVICES |
ICAS2012-3.10.4 |
| Thomson, D. G. |
ASSESSING
HELICOPTER SURVIVABILITY TO GROUND LAUNCHED PROJECTILES USING MULTI-FIDELITY
INVERSE SIMULATION |
ICAS2012-1.4.4 |
| Thomson, R. |
A FEASIBILITY STUDY FOR
MULTI-MATERIAL RETROFITTABLE ENERGY ABSORBING STRUCTURE FOR AGED HELICOPTER
SUBFLOOR |
ICAS2012-12.3.3 |
| Thomson, R. |
DIRECTIONAL ENHANCEMENT OF
COMPOSITE STRUCTURES ENERGY ABSORPTION USING MAGNETORHEOLOGICAL FLUIDS |
ICAS2012-7.8.1 |
| Thomson, R. |
IMPROVED DESIGN METHODS FOR
CRASHWORTHY COMPOSITE HELICOPTER STRUCTURES |
ICAS2012-8.1.2 |
| Thomson, R. |
EXPERIMENTAL DEVELOPMENT AND
ANALYSIS OF AN ACTIVE CRUSHING ELEMENT USING PRESSURIZED COMPOSITE TUBES |
ICAS2012-8.1.ST |
| Thouault, N. |
AEROACOUSTIC ANALYSIS OF A
HELICOPTER CONFIGURATION WITH DUCTED TAIL ROTOR |
ICAS2012-3.9.1 |
| Timokhin, V. |
AEROELASTIC
MULTIDISCIPLINARY ANALYSIS OF THE FIN
WITH INNOVATIVE ADAPTIVE CONTROL |
ICAS2012-8.7.4 |
| Tisato, J. |
APPLICATION OF THE RANGE
SAFETY TEMPLATE TOOLKIT TO UAS RISK HAZARD ANALYSES SUPPORTING AIRWORTHINESS
REGULATION |
ICAS2012-9.2.3 |
| Tobin, E. F. |
EVALUATION AND CORRELATION
OF INTER-LABORATORY RESULTS FROM A RAIN EROSION TEST CAMPAIGN |
ICAS2012-12.2.3 |
| Tobin, E. F. |
LABORATORY TESTING OF INSECT
CONTAMINATION FOR LAMINAR FLOW APPLICATIONS USING AN INSECT-IMPACT TEST
FACILITY |
ICAS2012-3.4.4 |
| Toebben, H. H. |
FLIGHT TESTING OF NOISE
ABATING RNP PROCEDURES AND STEEP APPROACHES |
ICAS2012-4.9.1 |
| Tokutake, H. |
THE FLAPPING AIRCRAFT
DYNAMICS WITH WING DEFORMATION UNDER GUST INPUT |
ICAS2012-11.9.2 |
| Tomczyk, A. |
CONTROL AUGMENTATION SYSTEM
FOR REMOTE STEERING UAV |
ICAS2012-6.9.3 |
| Tomczyk, A. |
MODEL FOLLOWING TOTAL IN
FLIGHT SIMULATOR AS AN EDUCATIONAL TOOL |
ICAS2012-P5.1 |
| Tong, L. |
DESIGN CONSIDERATIONS OF A
PRESSURE DRIVEN MORPHING WING STRUCTURE |
ICAS2012-8.4.1 |
| Toor, J. van |
VOLTAIR - THE ALL ELECTRIC
PROPULSION CONCEPT PLATFORM – A VISION FOR ATMOSPHERIC FRIENDLY FLIGHT |
ICAS2012-4.7.2 |
| Torabi, A. |
EFFECT OF LATERAL PLACEMENT
OF CERAMIC AND METAL GRAINS ON THERMAL STRESS DISTRIBUTION THROUGHOUT FGMS |
ICAS2012-7.3.4 |
| Toratani, D. |
RESEARCH AND DEVELOPMENT OF
DOUBLE TETRAHEDRON HEXA-ROTORCRAFT (DOT-HR) |
ICAS2012-1.4.2 |
| Toratani, D. |
COLLISION AVOIDANCE OF
INDOOR FLYING DOUBLE TETRAHEDRON HEXA-ROTORCRAFT |
ICAS2012-11.5.1 |
| Torii, H. |
THE EXTENSION OF
DISCRETE-TIME FLUTTER MARGIN |
ICAS2012-8.5.2 |
| Törner, S. |
IMPLEMENTING TIME BASED CDA
OPERATIONS IN A MEDIUM-HIGH DENSITY ATM ENVIRONMENT |
ICAS2012-10.8.1 |
| Toussaint, C. |
INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS2012-1.10.2 |
| Tran, T. |
APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS2012-8.9.2 |
| Travaglini, L. |
NEOCASS: AN OPEN SOURCE
ENVIRONMENT FOR THE AEROELASTIC ANALYSIS AT CONCEPTUAL DESIGN LEVEL |
ICAS2012-8.10.1 |
| Tripero, A. M. G. |
WEIGHT ON WHEEL SYSTEM BASED
ON STRAIN GAUGES |
ICAS2012-6.11.2 |
| Tristrant, D. |
FAULT DETECTION AND
RECONFIGURATION APPLIED TO A HELICOPTER SWASHPLATE ACTUATOR |
ICAS2012-5.1.2 |
| Troncone, E. |
IDENTIFICATION OF HELICOPTER
GROUND RESONANCE WITH MULTI-BODY SIMULATION |
ICAS2012-8.3.2 |
| Truss, R. |
INTERFACE DIFFUSION AND
MORPHOLOGY OF AEROSPACE GRADE EPOXY CO-CURED WITH THERMOPLASTIC POLYMERS |
ICAS2012-7.8.2 |
| Tshuchiya, T. |
FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS2012-5.2.1 |
| Tsourdos, A. |
MULTIPLE UAV FORMATION
RECONFIGURATION WITH COLLISION AVOIDANCE GUIDANCE VIA DIFFERENTIAL GEOMETRY
CONCEPT |
ICAS2012-11.2.2 |
| Tumanov, N. V. |
PREVENTION OF LOW CYCLE
FATIGUE FRACTURE OF AVIATION ENGINE CRITICAL PARTS |
ICAS2012-4.1.2 |
| Tupper, A. |
MANAGING DIFFUSE ERUPTION
CLOUDS - THE EXPERIENCES OF 2010-11, AND THE RESULTS OF THE INTERNATIONAL
VOLCANIC ASH TASK FORCE |
ICAS2012-0.7 |
| Tuss, J. |
A PLANAR ANTENNA ARRAY
MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC |
ICAS2012-6.11.ST |
| Tutty, M. G. |
A RECENT HISTORY OF THE
EVOLUTION OF AUSTRALIA’S AERODYNAMICS STORE SEPARATION CAPABILITY – THROUGH
INDIGENOUS AND INTERNATIONAL PROGRAMS |
ICAS2012-10.6.4 |
| Ubadike, O. C. |
FUZZY LOGIC BASED FLIGHT
CONTROL SYSTEM FOR THE NIGERIAN AIR FORCE AIR BEETLE AIRCRAFT |
ICAS2012-P5.12 |
| Ucan, H. |
SENSOR AND
REAL-TIME-PROCESS-SIMULATION GUIDED AUTOCLAVE PROCESS CONTROL FOR COMPOSITE
PRODUCTION |
ICAS2012-6.1.2 |
| Uchiumi, M. |
INTEGRATED DESIGN METHOD OF
A ROCKET ENGINE TURBOPUMP SUB-SYSTEM FOR SUPPRESSING ROTOR LATERAL VIBRATION |
ICAS2012-4.3.4 |
| Uchiyama, K. |
DESIGN OF ROBUST FLIGHT
CONTROL SYSTEM FOR SMALL FIXED-WING UAV |
ICAS2012-11.9.3 |
| Udzhukhu, A. Y. |
ADVANCED AEROSPACE SYSTEMS
WITH INTERCONTINENTAL AND GLOBAL RANGE OF FLIGHT |
ICAS2012-1.5.2 |
| Ueda, Y. |
STABILITY ANALYSIS ON
NATURAL LAMINAR FLOW WING IN SUPERSONIC FLOW: ONERA-JAXA JOINT RESEARCH
PROGRAM |
ICAS2012-3.10.1 |
| Uejima, K. |
ANALYZING SEPARATION LOSS
EVENTS IN TWO-PAIRED AIRCRAFT TRAILING CONDUCTING AIRBORNE TIME SPACING BASED
CONTINUOUS DESCENT ARRIVAL |
ICAS2012-10.8.3 |
| Ueno, A. |
SIMULTANEOUS OPTIMIZATION OF
AIRFRAME AND ENGINE FOR SUPERSONIC TRANSPORT |
ICAS2012-12.3.4 |
| Ueno, M. |
ANALYTIC METHOD FOR FLIGHT
MOTION OF AIRCRAFT WITH A SINGLE VIDEO CAMERA AND ITS APPLICATION TO A FREE
FLIGHT GLIDER |
ICAS2012-5.6.1 |
| Ueno, S. |
COLLISION AVOIDANCE OF
INDOOR FLYING DOUBLE TETRAHEDRON HEXA-ROTORCRAFT |
ICAS2012-11.5.1 |
| Uher, O. |
THE CFRP SAILPLANE WING
SEGMENTS MANUFACTURED BY FILAMENT PLACEMENT |
ICAS2012-7.5.ST |
| Unay, E. |
METHODS FOR EVALUATION OF
AIRCRAFT MASS DISTRIBUTION |
ICAS2012-1.1.3 |
| Unay, E. |
TOOL DEVELOPMENT FOR
AIRCRAFT LOADS POST-PROCESSING |
ICAS2012-P3.5 |
| Urik, T. |
THE CFRP SAILPLANE WING
SEGMENTS MANUFACTURED BY FILAMENT PLACEMENT |
ICAS2012-7.5.ST |
| Uspensky, A. A. |
INFLUENCE OF TURBULENCE
SCALE AND SHAPE OF LEADING EDGE ON FST-INDUCED LAMINAR-TURBULENT TRANSITION |
ICAS2012-2.4.3 |
| Ustinov, M. V. |
INFLUENCE OF TURBULENCE
SCALE AND SHAPE OF LEADING EDGE ON FST-INDUCED LAMINAR-TURBULENT TRANSITION |
ICAS2012-2.4.3 |
| Uzunoglu, A. |
TOOL DEVELOPMENT FOR
AIRCRAFT LOADS POST-PROCESSING |
ICAS2012-P3.5 |
| Vadillo, J. L. |
ACTIVE
CONTROL OF SHOCK/BOUNDARY LAYER INTERACTION FOR TRANSONIC DRAG REDUCTION OF
AIRFOILS |
ICAS2012-2.10.4 |
| Valiyff, A. |
FLEXIBILITY OF AN ORITHOPTER
WING TESTED IN A WIND-TUNNEL |
ICAS2012-12.5.3 |
| van den Berg, T. |
AUTOMATIC FLATTENING OF THREE-DIMENSIONAL WIRING HARNESSES FOR
MANUFACTURING |
ICAS2012-6.4.2 |
| Van den Brink, W. |
BUCKLING-OPTIMIZED VARIABLE
STIFFNESS LAMINATES FOR A COMPOSITE FUSELAGE WINDOW SECTION |
ICAS2012-8.9.3 |
| van der Hoogt, P. |
ACCELERATED LIFE CONSUMPTION
DUE TO THERMO-ACOUSTIC OSCILLATIONS IN GAS TURBINES: XFEM & CRACK |
ICAS2012-4.2.2 |
| van der Windt, M. |
CURFEWS AT INTERNATIONAL
AIRPORTS - A STUDY OF CURRENT PRACTICE |
ICAS2012-10.5.3 |
| van Dommelen, J. |
A CONCEPTUAL DESIGN AND
ANALYSIS TOOL FOR BLENDED WING BODY AIRCRAFT |
ICAS2012-1.7.2 |
| van Tooren, M. J. L. |
AUTOMATIC FLATTENING OF THREE-DIMENSIONAL WIRING HARNESSES FOR
MANUFACTURING |
ICAS2012-6.4.2 |
| Vandewater, L. A. |
BI-AXIAL VIBRATION ENERGY
HARVESTING FOR USE ON AEROSPACE PLATFORMS |
ICAS2012-6.7.1 |
| Vandi, L. -J. |
INTERFACE DIFFUSION AND
MORPHOLOGY OF AEROSPACE GRADE EPOXY CO-CURED WITH THERMOPLASTIC POLYMERS |
ICAS2012-7.8.2 |
| Vankan, W. J. |
BUCKLING-OPTIMIZED VARIABLE
STIFFNESS LAMINATES FOR A COMPOSITE FUSELAGE WINDOW SECTION |
ICAS2012-8.9.3 |
| Vanneste, T. |
AEROELASTIC SIMULATION OF
FLEXIBLE FLAPPING WING BASED ON STRUCTURAL FEM AND QUASI-STEADY AERODYNAMIC
MODEL |
ICAS2012-8.5.1 |
| Vanuchi, P. |
WIND TUNNEL TESTING OF
POROUS DEVICES FOR THE REDUCTION OF FLAP SIDE-EDGE NOISE |
ICAS2012-9.11.2 |
| Varley, R. V. |
DELAMINATION TOUGHENING OF
CARBON-EPOXY LAMINATE WITH A POLYETHYLENE-CO-METHACRYLIC ACID (EMAA)
SELF-HEALING MODIFIER |
ICAS2012-7.6.2 |
| Vasiliev, V. V. |
DEVELOPMENT OF GEODESIC
COMPOSITE AIRCRAFT STRUCTURES |
ICAS2012-8.4.2 |
| Vasilyev, B. |
PREDICTION OF THE KINETICS
OF THE 3D STRESS-STRAIN STATE OF HIGH-TEMPERATURE GAS TURBINE BLADES WITH
LIMITED EXPERIMENTAL DATA |
ICAS2012-4.2.1 |
| Vasista, S. |
DESIGN CONSIDERATIONS OF A
PRESSURE DRIVEN MORPHING WING STRUCTURE |
ICAS2012-8.4.1 |
| Vaughn, L. |
COMPOSITE SANDWICH PANEL
BIRDSTRIKE TESTING AND ANALYSIS |
ICAS2012-8.3.4 |
| Vedeshkin, G. K. |
EXPERIMENTAL INVESTIGATIONS
OF HYDRAULIC DEVICES PERFORMANCE IN AVIATION ENGINE COMPARTMENT |
ICAS2012-P2.10 |
| Veidt, M. |
FINITE ELEMENT SIMULATION OF
CRACK PROPAGATION IN MILITARY AIRCRAFT COATINGS |
ICAS2012-7.2.3 |
| Veidt, M. |
INTERFACE DIFFUSION AND
MORPHOLOGY OF AEROSPACE GRADE EPOXY CO-CURED WITH THERMOPLASTIC POLYMERS |
ICAS2012-7.8.2 |
| Veldhuis, L. |
PROPELLER INDUCED GROUND
VORTEX |
ICAS2012-4.10.3 |
| Veldhuis, L. L. M. |
NOVEL PASSIVE AND ACTIVE
FLOW CONTROL FOR HIGH LIFT |
ICAS2012-3.7.2 |
| Venediktov, V. D. |
INTERDISCIPLINARY COMPLEX
DESIGN OF MODERN HIGH AND LOW PRESSURE TURBINES |
ICAS2012-4.3.3 |
| Venediktov, V. D. |
THE EXPERIENCE OF HIGH
PRESSURE RATIO SINGLE STAGE HPT DESIGNING |
ICAS2012-P4.15 |
| Venkatraman, K. |
TRANSONIC FLUTTER, SHOCKS,
AND PARAMETER EFFECTS |
ICAS2012-2.6.4 |
| Verseux, O. |
EXPERIMENTAL INVESTIGATIONS
OF HYDRAULIC DEVICES PERFORMANCE IN AVIATION ENGINE COMPARTMENT |
ICAS2012-P2.10 |
| Verstraete, D. |
PRELIMINARY DESIGN OF A
FUEL-CELL-BASED HYBRID-ELECTRICAL UAV |
ICAS2012-1.8.2 |
| Verstraete, D. |
DESIGN AND TEST OF A UAV
BLENDED WING BODY CONFIGURATION |
ICAS2012-1.8.3 |
| Verstraete, D. |
HARDWARE-IN-THE-LOOP
SIMULATION OF FUEL-CELL-BASED HYBRID-ELECTRICAL UAV PROPULSION |
ICAS2012-4.5.2 |
| Verstraete, D. |
DESIGN AND AERO-ELASTIC
OPTIMISATION OF THE STRUCTURE OF THE LAPCAT A2 MACH 5 AIRLINER |
ICAS2012-8.4.3 |
| Verstraete, D. |
DEVELOPMENT OF A
HYBRID-ELECTRIC POWER-SYSTEM MODEL FOR A SMALL SURVEILLANCE AIRCRAFT |
ICAS2012-P6.4 |
| Vich, O. |
EIGENVALUE AND FLUTTER
SENSITIVITY ANALYSIS OF AIRLINER WING |
ICAS2012-P3.1 |
| Ville, F. |
COUPLING MECH. & THERMAL
MODELS IN PRELIMINARY DESIGN OF POWER TRANSMISSIONS DRIVEN BY THERMAL ISSUES |
ICAS2012-6.6.1 |
| Vine, J. |
LOAD SYNTHESIS OF HELICOPTER
DYNAMIC COMPONENTS: IMPROVEMENTS TO LINEAR REGRESSION IN THE AZIMUTH DOMAIN |
ICAS2012-8.10.ST |
| Vio, G. A. |
NON-LINEAR BEHAVIOUR OF A
WING DUE TO UNDERWING STORES |
ICAS2012-10.6.ST2 |
| Vio, G. A. |
DESIGN OF COMPOSITE
STRUCTURES FOR IMPROVED AEROELASTIC PERFORMANCE |
ICAS2012-8.4.4 |
| Vio, G. A. |
AEROELASTIC RESPONSE OF A
CHORDWISE FLEXIBLE WINGS SUBJECTED TO GUSTS: AN INITIAL STUDY ON EXPERIMENTAL
AND COMPUTATIONAL VALIDATION |
ICAS2012-8.5.3 |
| Viviani, A. |
DESIGN OF MASS SAVING
CONFIGURATIONS FOR WINGED REENTRY VEHICLES |
ICAS2012-1.5.3 |
| Viviani, A. |
AEROTHERMODYNAMIC FIELD PAST
A REENTRY CAPSULE FOR SAMPLE RETURN MISSIONS |
ICAS2012-3.8.1 |
| Vlasenko, V. V. |
APPLICATION OF THE FAST
CALCULATION TECHNOLOGIES TO SIMULATION OF NON-STATIONARY SUPERSONIC VISCID
FLOW WITH COMBUSTION |
ICAS2012-6.2.3 |
| Voevodenko, N. V. |
NUMERICAL RESEARCH OF THE
AIR INTAKE LOCATION INFLUENCE ONTO THE HIGH-SPEED AIRCRAFT PERFORMANCE |
ICAS2012-P2.1 |
| Vogel, M. |
INVESTIGATING THE SAFETY
IMPACT OF TIME BUFFERS IN CURRENT TMA ARRIVAL OPERATIONS |
ICAS2012-9.4.3 |
| Voges, V. |
APPLICATION AND POTENTIALS
OF WIRELESS COMMUNICATION TECHNOLOGIES IN PASSENGER AIR TRANSPORT FROM AN
AVIATION SECURITY STANDPOINT |
ICAS2012-9.6.3 |
| Voggenreiter, H. |
NUMERICAL SIMULATIONS AND
EXPERIMENTAL INVESTIGATIONS ON QUASI-STATIC AND CYCLIC MIXED MODE
DELAMINATION OF MULTIDIRECTIONAL CFRP LAMINATES |
ICAS2012-7.4.2 |
| Vörsmann, P. |
OPTIMIZATION OF A NEW
MULTI-PURPOSE UAS FOR SCIENTIFIC APPLICATIONS USING AERODYNAMIC
RECONFIGURATION |
ICAS2012-11.6.4 |
| Vos, J. |
SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS2012-10.6.1 |
| Vos, R. |
A CONCEPTUAL DESIGN AND
ANALYSIS TOOL FOR BLENDED WING BODY AIRCRAFT |
ICAS2012-1.7.2 |
| Voyevodin, A. V. |
EXPERIMENTAL AND NUMERICAL
INVESTIGATIONS OF LOCAL AERODYNAMICS OF CIVIL AIRCRAFT |
ICAS2012-2.9.4 |
| Vrchota, P. |
WIND TUNNEL AND CFD STUDY OF
AIRFOIL WITH AIRBRAKE |
ICAS2012-10.6.ST1 |
| Vrchota, P. |
GLOBAL OPTIMIZATION OF
TWO-DIMENSIONAL HIGH LIFT AERODYNAMIC SYSTEM |
ICAS2012-11.10.2 |
| Vu, N. A. |
AN INTEGRATED FRAMEWORK FOR
INNOVATIVE COMPOUND GYROPLANE DESIGN SYSTEM |
ICAS2012-1.4.ST |
| Vuletich, I. |
APPLICATION OF THE RANGE
SAFETY TEMPLATE TOOLKIT TO UAS RISK HAZARD ANALYSES SUPPORTING AIRWORTHINESS
REGULATION |
ICAS2012-9.2.3 |
| Wadia, A. R. |
THE EFFECT OF PLASMA
ACTUATORS ON TIP CLEARANCE FLOWS IN COMPRESSOR ROTORS |
ICAS2012-4.4.1 |
| Wadsley, B. |
SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS2012-7.2.2 |
| Wagner, M. |
MULTIDISCIPLINARY AIRFRAME
DESIGN OPTIMIZATION |
ICAS2012-0.4 |
| Wainwright, A. |
FIELD-OF-VIEW, DETECTION
RANGE, AND FALSE ALARM TRADE-OFFS IN VISION-BASED AIRCRAFT DETECTION |
ICAS2012-6.9.1 |
| Waitman, S. |
AUTOPILOT
DESIGN FOR THE EOLE DEMONSTRATOR |
ICAS2012-5.3.4 |
| Walker, R. |
FIELD-OF-VIEW, DETECTION
RANGE, AND FALSE ALARM TRADE-OFFS IN VISION-BASED AIRCRAFT DETECTION |
ICAS2012-6.9.1 |
| Wan, T. |
AERODYNAMIC
ANALYSIS OF 3-D FLAPPING WING MOTION VIA THE HILBERT-HUANG TRANSFORM METHOD |
ICAS2012-9.8.ST |
| Wang, B. |
STUDY ON THE FLOW STRUCTURES
OF THE SHOCKWAVE AND TURBULENT BOUNDARY-LAYER INTERACTION |
ICAS2012-11.4.3 |
| Wang, B. |
NUMERICAL SIMULATIONS OF
SELF-SUSTAINED AEROELASTIC OSCILLATIONS AT LOW REYNOLDS NUMBERS |
ICAS2012-2.6.3 |
| Wang, B. |
SIZE EFFECT OF FAILURE MODES
IN COMPOSITE LAMINATES UNDER COMPRESSION |
ICAS2012-7.4.3 |
| Wang, B. |
POST-BUCKLING
BEHAVIOR OF LAMINATED STRINGER STIFFENED PANEL UNDER COMPRESSIVE
LOAD—EXPERIMENTS AND ANALYSIS |
ICAS2012-7.4.4 |
| Wang, C. |
STEADY
AND UNSTEADY FLOWS PAST AIRFOILS AT LOW REYNOLDS NUMBERS IN THE PROXIMITY OF
THE GROUND |
ICAS2012-3.6.ST |
| Wang, C. H. |
EFFECT OF OFF-NORMAL LOADING
ON THE BOND STRENGTH MEASUREMENT OF BONDED REPAIRS |
ICAS2012-12.2.1 |
| Wang, C. H. |
CRITICAL ASSESSMENT OF
FAILURE CRITERION FOR ADHESIVELY BONDED COMPOSITE JOINT REPAIR DESIGN |
ICAS2012-12.2.2 |
| Wang, C. H. |
DELAMINATION TOUGHENING OF
CARBON-EPOXY LAMINATE WITH A POLYETHYLENE-CO-METHACRYLIC ACID (EMAA)
SELF-HEALING MODIFIER |
ICAS2012-7.6.2 |
| Wang, C. H. |
INVESTIGATION INTO OPTIMISED
COMPOSITE SCARF REPAIRS WITH PRACTICAL CONSTRAINTS |
ICAS2012-P3.4 |
| Wang, H. J. |
AERODYNAMIC
DESIGN OF PROPELLER FOR LONG ENDURANCE |
ICAS2012-4.5.3 |
| Wang, H. S. |
STRUCTURAL
INTEGRITY ANALYSIS AND TEST OF FATIGUE CRITICAL LOCATION OF MA60 REGIONAL JET |
ICAS2012-7.9.4 |
| Wang, J. |
ANALYZING AND MODELING OF
JAMMING DESTROY FACTOR |
ICAS2012-P6.1 |
| Wang, J. J. |
THE DYNAMIC BEHAVIOR OF
FUNCTIONALLY GRADED PLATES UNDER THE IMPACT LOADING |
ICAS2012-7.7.3 |
| Wang, L. J. |
INVESTIGATION IN THE DYNAMIC
FORCE EQUALIZATION OF DISSIMILAR REDUNDANT ACTUATION SYSTEMS OPERATING IN
ACTIVE/ACTIVE MODE |
ICAS2012-6.8.1 |
| Wang, Z. |
PREDICTING NOISE EXPOSURE
FOR FLIGHT CREW MEMBERS |
ICAS2012-7.10.5 |
| Watanabe, S. |
NUMERICAL STUDY OF THE
EFFECTS OF CROSS-WIND ON THE JET BLAST DEFORMATION |
ICAS2012-10.10.3 |
| Watanabe, Y. |
SIMULTANEOUS OPTIMIZATION OF
AIRFRAME AND ENGINE FOR SUPERSONIC TRANSPORT |
ICAS2012-12.3.4 |
| Watanabe, Y. |
EXPERIMENTAL STUDY OF
SUPERSONIC INLET FOR SUPPRESSION OF BUZZ IN SUBCRITICAL OPERATION |
ICAS2012-6.2.1 |
| Watanabe, Y. |
PERFORMANCE EVALUATION OF A
BOUNDARY-LAYER DIVERTER FOR SUPERSONIC PROPULSION SYSTEM |
ICAS2012-6.2.2 |
| Waterhouse, J. R. |
THE INFLUENCE OF DEMOISELLE
AIRCRAFT ON LIGHT AND GENERAL AVIATION DESIGN |
ICAS2012-1.7.ST |
| Watkins, S. |
THE INFLUENCE OF TURBULENCE
INTENSITY ON THE FLOW STRUCTURE OVER A THIN AIRFOIL AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.2 |
| Watkins, S. |
OPTIMUM LOCATION OF PRESSURE
MEASUREMENTS AROUND A WING AS A DYNAMIC CONTROL INPUT IN SMOOTH AND TURBULENT
CONDITIONS |
ICAS2012-3.3.3 |
| Watkins, S. |
FLOW-INDUCED FLUTTER OF
SLENDER CANTILEVER HIGH-COMPLIANCE PLATES |
ICAS2012-8.10.5 |
| Watkins, S. |
DYNAMIC SURFACE PRESSURE
MEASUREMENTS ON A FLAPPING WING IN SMOOTH AND TURBULENT FLOW |
ICAS2012-9.11.ST1 |
| Watmuff, J. |
THE INFLUENCE OF TURBULENCE
INTENSITY ON THE FLOW STRUCTURE OVER A THIN AIRFOIL AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.2 |
| Watmuff, J. |
DYNAMIC SURFACE PRESSURE
MEASUREMENTS ON A FLAPPING WING IN SMOOTH AND TURBULENT FLOW |
ICAS2012-9.11.ST1 |
| Wei, A. K. L. |
CONCEPTUAL DESIGN AND
AERODYNAMIC STUDY OF BLENDED WING BODY BUSINESS JET |
ICAS2012-2.9.2 |
| Wei, Y. |
SIZE EFFECT OF FAILURE MODES
IN COMPOSITE LAMINATES UNDER COMPRESSION |
ICAS2012-7.4.3 |
| Weinerfelt, P. |
A COUPLED AERO AND
STRUCTURAL DYNAMICS MODEL FOR COMPUTATION OF UNSTEADY LOADS ON THE HELICOPTER
SKELDAR V200 |
ICAS2012-8.7.2 |
| Weiss, M. |
TECHNOLOGY ASSESSMENT OF
FUTURE AIRCRAFT: SOCIO-ECO-EFFICIENCY IN CONCEPTUAL AIRCRAFT DESIGN |
ICAS2012-1.9.2 |
| Wentink, M. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
| Westphal, J. |
OPERATIONAL
HUMAN-IN-THE-LOOP INTEGRATION OF 4D ARRIVAL GUIDANCE |
ICAS2012-5.8.1 |
| Wheatley, B. J. |
TUNABLE DIODE LASER
ABSORPTION SPECTROSCOPY OF HYPERSONIC FLOWS |
ICAS2012-4.8.2 |
| Wheatley, V. |
THERMAL NON-EQUILIBRIUM
EFFECTS IN RADICAL FARMING SCRAMJETS |
ICAS2012-11.4.1 |
| Wheatley, V. |
STREAMWISE PORTHOLE FUEL
INJECTION FOR BOUNDARY-LAYER COMBUSTION INSIDE A SCRAMJET ENGINE |
ICAS 2012-P4.16 |
| Wheatley, V. |
JET INTERACTION IN A
HYPERSONIC FLOW: A COMPARISON BETWEEN PLIF THERMOMETRY AND COMPUTATIONAL
SIMULATION |
ICAS2012-4.11.2 |
| White, B. |
MULTIPLE UAV FORMATION
RECONFIGURATION WITH COLLISION AVOIDANCE GUIDANCE VIA DIFFERENTIAL GEOMETRY
CONCEPT |
ICAS2012-11.2.2 |
| Wiart, L. |
AUTOMATED CHAIN FOR
AERODYNAMIC COMPUTATIONS MEETING AIRCRAFT TRIMMING REQUIREMENTS |
ICAS2012-2.10.1 |
| Wicke, K. |
MISSION AND ECONOMIC
ANALYSIS OF AIRCRAFT WITH NATURAL LAMINAR FLOW TECHNOLOGY |
ICAS2012-1.7.4 |
| Wickramasinghe, N. K. |
FLIGHT TRAJECTORY
OPTIMIZATION FOR AN EFFICIENT AIR TRANSPORTATION SYSTEM |
ICAS2012-5.8.3 |
| Widjanarko, S. M. D. |
EXPERIMENTAL/NUMERICAL
INVESTIGATION AIRFOIL WITH FLOW CONTROL BY SYNTHETIC JETS |
ICAS2012-3.7.5 |
| Wieczorek, K. |
MULTI-DISCIPLINARY DESIGN
AND FEASIBILITY STUDY OF DISTRIBUTED PROPULSION SYSTEMS |
ICAS2012-1.7.5 |
| Wiedemann, M. |
SENSOR AND
REAL-TIME-PROCESS-SIMULATION GUIDED AUTOCLAVE PROCESS CONTROL FOR COMPOSITE
PRODUCTION |
ICAS2012-6.1.2 |
| Wild, G. |
ACOUSTIC
POWER AND DATA FOR MORE ROBUST FLIGHT DATA AND COCKPIT VOICE RECORDERS |
ICAS2012-6.10.5 |
| Wild, G. |
DISTRIBUTED
OPTICAL FIBRE SMART SENSORS FOR ADVANCE SENSING SYSTEMS IN AEROSPACE VEHICLES |
ICAS2012-P6.7 |
| Williams, B. |
COMPUTATIONAL ASPECTS OF
PROBABILISTIC ASSESSMENT OF UAS ROBUST AUTONOMY |
ICAS2012-9.2.2 |
| Williams, B. |
EVALUATION OF ROBUST
AUTONOMY AND IMPLICATIONS ON UAS DESIGN |
ICAS2012-9.4.2 |
| Williams, P. |
ALL-SOURCE NAVIGATION FOR
ENHANCING UAV OPERATIONS IN GPS-DENIED ENVIRONMENTS |
ICAS2012-11.6.1 |
| Williams, P. |
INTELLIGENT LANDING SYSTEM
FOR LANDING UAVS AT UNSURVEYED AIRFIELDS |
ICAS2012-11.6.2 |
| Williams, W. |
APPLICATION OF THE RANGE
SAFETY TEMPLATE TOOLKIT TO UAS RISK HAZARD ANALYSES SUPPORTING AIRWORTHINESS
REGULATION |
ICAS2012-9.2.3 |
| Wilson, M. |
GROUND-BASED SENSE AND AVOID
SUPPORT FOR UNMANNED AIRCRAFT SYSTEMS |
ICAS2012-11.3.3 |
| Wilson, M. |
THE SMART SKIES PROJECT:
ENABLING TECHNOLOGIES FOR FUTURE AIRSPACE ENVIRONMENTS |
ICAS2012-6.9.2 |
| Wilson, S. |
APPLICATION OF THE RANGE
SAFETY TEMPLATE TOOLKIT TO UAS RISK HAZARD ANALYSES SUPPORTING AIRWORTHINESS
REGULATION |
ICAS2012-9.2.3 |
| Winship, S. |
FIRE-X
407 DEVELOPMENT: UNMANNING THE BELL HELICOPTER 407 WITH THE US NAVY FIRE
SCOUT MQ-8B AUTONOMOUS SYSTEM |
ICAS2012-P1.1 |
| Witte, P. |
A NON-WEIGHT BASED,
MANUFACTURING INFLUENCED DESIGN (MIND) METHODOLOGY FOR PRELIMINARY DESIGN |
ICAS2012-6.4.3 |
| Wolters, F. |
IMPACT OF ALTERNATIVE FUELS
ON ENGINE PERFORMANCE AND CO2-EMISSIONS |
ICAS2012-8.6.3 |
| Won, D. -Y. |
HIDDEN MARKOV MODEL
PARAMETER ESTIMATION FOR MULTIPLE DIM TARGET DETECTION |
ICAS2012-P6.5 |
| Wong, A. K. |
MAKING THE INVISIBLE
VISIBLE: JOINING THE DOTS FROM LORD KELVIN TO FIGHTER JET FATIGUE |
ICAS2012-8.2.3 |
| Wong, K. C. |
INVESTIGATION OF LOW THRUST
TO WEIGHT RATIO ROTATIONAL CAPACITY OF ASYMMETRIC MONO-WING CONFIGURATIONS |
ICAS2012-1.4.3 |
| Wong, K. C. |
DESIGN AND TEST OF A UAV
BLENDED WING BODY CONFIGURATION |
ICAS2012-1.8.3 |
| Worotynska, J. |
AEROELASTIC RESPONSE OF A
CHORDWISE FLEXIBLE WINGS SUBJECTED TO GUSTS: AN INITIAL STUDY ON EXPERIMENTAL
AND COMPUTATIONAL VALIDATION |
ICAS2012-8.5.3 |
| Wright, L. M. |
DEVELOPMENT OF AN
EXPERIMENTAL TECHNIQUE FOR HIGH TEMPERATURE IMPINGEMENT STUDIES |
ICAS2012-12.6.3 |
| Wroblewski, W. |
A HIGHLY EXPANDABLE LOW-COST
OPEN-SOURCE UAV SYSTEM WITH HIGH ON-BOARD PROCESSING POWER |
ICAS2012-1.8.1 |
| Wu, S.-C. |
PILOT CONVECTIVE WEATHER
DECISION MAKING IN EN ROUTE AIRSPACE |
ICAS2012-10.4.3 |
| Wu, X. R. |
ANALYSIS OF MULTIPLE SITE
DAMAGE IN AIRCRAFT STRUCTURES BY USING WEIGHT FUNCTION METHOD IN FRACTURE
MECHANICS |
ICAS2012-7.1.1 |
| Wu, X. R. |
LCF BEHAVIOR AND LIFE
EVALUATION OF A SINGLE CRYSTAL NICKEL BASE SUPERALLOY UNDER DIFFERENT DWELL
CONDITION |
ICAS2012-7.3.3 |
| Xia, L. |
IMPROVED PARTICLE SWARM
OPTIMIZATION BASED ON SOCIAL MODEL FOR AERODYNAMIC DESIGN |
ICAS2012-11.10.4 |
| Xia, M. |
NUMERICAL STUDY OF PITCHING
OSCILLATION EFFECT ON AERODYNAMIC CHARACTERISTICS OVER ASYMMETRIC VORTEX
STRUCTURE OF SLENDER REVOLUTION |
ICAS2012-2.5.2 |
| Xia, Z. F. |
TIME-ACCURATE VERSUS
ACTUATOR DISK SIMULATIONS OF PROPELLER SLIPSTREAM FLOWS |
ICAS2012-9.8.2 |
| Xiao, J. |
CONTROL-ORIENTED MODELING
AND ANALYSIS OF AERO-THERMO-ELASTIC-PROPULSION HYPERSONIC VEHICLE |
ICAS2012-1.5.1 |
| Xiao, Z.. X. |
INVESTIGATION OF PASSIVE
FLOW CONTROL METHODOLOGIES USING SST-IDDES |
ICAS2012-P2.7 |
| Xiong, C. |
CRACK NUCLEATION MODELING IN
NOTCHED SPECIMEN SUBJECTED TO HIGH FATIGUE LOADING |
ICAS2012-7.7.4 |
| Xiong, Q. |
THE WORKFLOW CONSTRUCTION
AND MANAGEMENT IN AERONAUTICAL MULTIDISCIPLINARY OPTIMIZATION |
ICAS2012-2.1.2 |
| Xiong, Q. |
THE METHOD FOR NONLINEAR
ANALYSIS OPTIMIZATION IN AERONAUTICAL RESEARCH |
ICAS2012-P1.2 |
| Xiong, W. |
POST-BUCKLING
BEHAVIOR OF LAMINATED STRINGER STIFFENED PANEL UNDER COMPRESSIVE
LOAD—EXPERIMENTS AND ANALYSIS |
ICAS2012-7.4.4 |
| Xu, F. |
SIZE EFFECT OF FAILURE MODES
IN COMPOSITE LAMINATES UNDER COMPRESSION |
ICAS2012-7.4.3 |
| Xu, G. Q. |
STUDY OF THE PRESSURE DROP
FOR RADIAL INFLOW BETWEEN CO-ROTATING DISCS |
ICAS2012-4.4.ST |
| Xu, R. F. |
MULTI-OBJECTIVE AERODYNAMIC
OPTIMIZATION DESIGN OF MULTI-ELEMENT AIRFOIL USING KRIGING MODEL |
ICAS2012-2.3.ST |
| Xu, W. |
ANALYSIS OF MULTIPLE SITE
DAMAGE IN AIRCRAFT STRUCTURES BY USING WEIGHT FUNCTION METHOD IN FRACTURE
MECHANICS |
ICAS2012-7.1.1 |
| Xu, X. W. |
RESEARCH ON METHODS OF
DYNAMIC MODELING AND SIMULATION FOR MORPHING WING AIRCRAFT |
ICAS2012-5.10.ST |
| Xu, Y. |
JET
NOISE REDUCTION BY MICROJETS |
ICAS2012-P4.2 |
| Xue, J. |
A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
| Xue, P. |
NUMERICAL
SIMULATION OF BIRD-STRIKING PROCESS AND ITS EXPERIMENTAL VERIFICATION |
ICAS2012-8.9.4 |
| Yadlin, Y. |
HIGH-LIFT SYSTEMS FOR
ENHANCED TAKEOFF PERFORMANCE |
ICAS2012-9.5.1 |
| Yakimenko, O. A. |
EXTENDING AUTONOMY
CAPABILITIES FOR UNMANNED SYSTEMS WITH CRUSER |
ICAS2012-11.6.3 |
| Yakushev, V. |
METHODS AND FACILITIES TO BE
USED TO EVALUATE THE AIRCRAFT FLIGHT AND NAVIGATION EQUIPMENT IN FLIGHT TESTS |
ICAS2012-5.6.3 |
| Yamada, G. |
ANALYTIC METHOD FOR FLIGHT
MOTION OF AIRCRAFT WITH A SINGLE VIDEO CAMERA AND ITS APPLICATION TO A FREE
FLIGHT GLIDER |
ICAS2012-5.6.1 |
| Yamada, T. |
EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS2012-9.3.1 |
| Yamamoto, I. |
DEVELOPMENT OF OBSERVATIONAL
SYSTEM WITH UNMANNED FLIGHT SYSTEM |
ICAS2012-P5.10 |
| Yamamoto, K. |
COMPUTATIONAL STUDY ON NOISE
GENERATION FROM A TWO-WHEEL MAIN LANDING GEAR |
ICAS2012-3.9.3 |
| Yamashita, Y. |
EXPERIMENTAL STUDY OF THE
MORPHING FLAP AS A LOW NOISE HIGH LIFT DEVICE FOR AIRCRAFT WING |
ICAS2012-9.11.3 |
| Yan, S. W. |
STUDY
ON MODELING PILOT BEHAVIOR BY ARTIFICIAL NEURAL NETWORK |
ICAS2012-5.9.ST |
| Yan, W. -Y. |
NUMERICAL STUDY ON RESIDUAL
THERMAL STRESSES IN CARBON FIBRE PULLOUT |
ICAS2012-7.3.1 |
| Yana, J. F. M |
PERFORMANCE ANALYSIS OF A
COAXIAL ROTOR SYSTEM IN HOVER: THREE POINTS OF VIEW |
ICAS2012-2.7.4 |
| Yanagida, A. |
FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS2012-5.2.1 |
| Yang, H. |
LAMINAR FLOW WING’S
OPTIMIZATION DESIGN BY RANS SOLVER WITH AUTOMATIC TRANSITION PREDICTION |
ICAS2012-2.2.3 |
| Yang, J. |
POST-BUCKLING
BEHAVIOR OF LAMINATED STRINGER STIFFENED PANEL UNDER COMPRESSIVE
LOAD—EXPERIMENTS AND ANALYSIS |
ICAS2012-7.4.4 |
| Yang, Q. |
A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
| Yang, S. P. |
ANALYSIS
OF FLUCTUATING LOAD OF A CIRCULAR CYLINDER UNDER THE FUSELAGE |
ICAS2012-P2.17 |
| Yang, S. -P. |
A PRELIMINARY CFD
INVESTIGATION ON REAR FUSELAGE SUPPORT CORRECTION |
ICAS2012-P2.14 |
| Yang, X. |
EXTRACTING DECK TREND TO
PLAN DESCENT TRAJECTORY FOR SAFE LANDING OF UAVS |
ICAS2012-11.8.3 |
| Yang, X. G. |
DETERMINATION OF AIRBORNE
RECORDED PARAMETERS FOR COMPREHENSIVE FLIGHT DATA MONITORING PROGRAM |
ICAS2012-9.4.1 |
| Yang, Y. |
INFLUENCE OF FLAPPING WING
UNSTEADY MOTION ON AERODYNAMIC PERFORMANCE OF HORIZONTAL TAIL |
ICAS2012-2.7.5 |
| Yang, Y. |
PROPELLER INDUCED GROUND
VORTEX |
ICAS2012-4.10.3 |
| Yang, Y. |
TIME-ACCURATE VERSUS
ACTUATOR DISK SIMULATIONS OF PROPELLER SLIPSTREAM FLOWS |
ICAS2012-9.8.2 |
| Yanovskiy, L. S. |
FUEL CELLS ON ALTERNATIVE
NON – OIL FUELS FOR GAS TURBINE ENGINES OF AN ADVANCED CIVIL AIRCRAFTS |
ICAS2012-P4.14 |
| Yao, Z. X. |
RESEARCH ON OPTIMIZING
ASCENT TRAJECTORY OF AERO-SPACE PLANE BASED ON COMBINED CYCLE PROPULSION |
ICAS2012-5.7.1 |
| Yarlagadda, P. |
A MICRO-SIMULATION OF
AIRPORT PASSENGERS WITH ADVANCED TRAITS |
ICAS2012-10.9.4 |
| Yashin, Y. P. |
EFFECTS OF MANIPULATOR TYPE
AND FEEL SYSTEM CHARACTERISTICS ON HIGH-FREQUENCY BIODYNAMIC PILOT-AIRCRAFT
INTERACTION |
ICAS2012-5.9.3 |
| Yashin, Y. P. |
SOME ASPECTS OF MOVING-BASE
SIMULATION OF UPSET RECOVERING MANEUVER |
ICAS2012-5.9.4 |
| Yeo, E. |
EFFECT OF OFF-NORMAL LOADING
ON THE BOND STRENGTH MEASUREMENT OF BONDED REPAIRS |
ICAS2012-12.2.1 |
| Yi, J. J. |
THERMAL ANALYSIS NEAR
SECONDARY INJECTION HOLE IN SITVC SYSTEM |
ICAS2012-P4.9 |
| Yokokawa, Y. |
COMPUTATIONAL STUDY ON NOISE
GENERATION FROM A TWO-WHEEL MAIN LANDING GEAR |
ICAS2012-3.9.3 |
| Yokozeki, T. |
TITANIUM METAL MATRIX
COMPOSITE DEVELOPMENT FOR COMMERCIAL AIRCRAFT LANDING GEAR STRUCTURE |
ICAS2012-7.5.1 |
| Yoo, D. -W. |
CONTROLLER DESIGN AND
ANALYSIS OF UNMANNED AERIAL VEHICLES USING AUTOMATIC GAIN GENERATION
TECHNIQUE |
ICAS2012-11.8.1 |
| Yoo, S. -J. |
AEROELASTIC ANALYSIS FOR
HELICOPTER ROTOR BLADES IN HOVER AND FORWARD FLIGHTS |
ICAS2012-11.5.3 |
| Yoshida, K. |
D-SEND PROJECT FOR LOW SONIC
BOOM DESIGN TECHNOLOGY |
ICAS2012-1.2.1 |
| Yoshida, K. |
DEVELOPMENT OF SUPERSONIC
NATURAL LAMINAR FLOW WING DESIGN SYSTEM USING CFD-BASED INVERSE METHOD |
ICAS2012-2.2.1 |
| Yoshida, K. |
STABILITY ANALYSIS ON
NATURAL LAMINAR FLOW WING IN SUPERSONIC FLOW: ONERA-JAXA JOINT RESEARCH
PROGRAM |
ICAS2012-3.10.1 |
| Yoshida, K. |
TITANIUM METAL MATRIX
COMPOSITE DEVELOPMENT FOR COMMERCIAL AIRCRAFT LANDING GEAR STRUCTURE |
ICAS2012-7.5.1 |
| Yoshida, Y. |
INTEGRATED DESIGN METHOD OF
A ROCKET ENGINE TURBOPUMP SUB-SYSTEM FOR SUPPRESSING ROTOR LATERAL VIBRATION |
ICAS2012-4.3.4 |
| Yoshihara, T. |
GBAS CURVED APPROACH
PROCEDURES: ADVANTAGES, CHALLENGES AND APPLICABILITY |
ICAS2012-4.9.2 |
| You, J. H. |
AEROACOUSTIC ANALYSIS OF A
HELICOPTER CONFIGURATION WITH DUCTED TAIL ROTOR |
ICAS2012-3.9.1 |
| Young, T. M. |
EVALUATION AND CORRELATION
OF INTER-LABORATORY RESULTS FROM A RAIN EROSION TEST CAMPAIGN |
ICAS2012-12.2.3 |
| Young, T. M. |
LABORATORY TESTING OF INSECT
CONTAMINATION FOR LAMINAR FLOW APPLICATIONS USING AN INSECT-IMPACT TEST
FACILITY |
ICAS2012-3.4.4 |
| Yu, H. C. |
LCF BEHAVIOR AND LIFE
EVALUATION OF A SINGLE CRYSTAL NICKEL BASE SUPERALLOY UNDER DIFFERENT DWELL
CONDITION |
ICAS2012-7.3.3 |
| Yu, J. G. |
FLOW
CONTROL TEST RESEARCH OF AIRCRAFT MODEL WITH ADJUSTABLE CANAEDS |
ICAS2012-P2.5 |
| Yu, M. S. |
THERMAL ANALYSIS NEAR
SECONDARY INJECTION HOLE IN SITVC SYSTEM |
ICAS2012-P4.9 |
| Yu, X. |
STUDY OF THE PRESSURE DROP
FOR RADIAL INFLOW BETWEEN CO-ROTATING DISCS |
ICAS2012-4.4.ST |
| Yu, X. |
LOAD SYNTHESIS OF HELICOPTER
DYNAMIC COMPONENTS: IMPROVEMENTS TO LINEAR REGRESSION IN THE AZIMUTH DOMAIN |
ICAS2012-8.10.ST |
| Yuan, W. |
DESIGN OF A mu SYNTHESIS
CONTROLLER TO STABILIZE AN UNMANNED HELICOPTER |
ICAS2012-11.5.2 |
| Yuan, W. |
A GREY-BOX SYSTEM
IDENTIFICATION PROCEDURE FOR SCALE MODEL HELICOPTERS BASED ON
FREQUENCY-DOMAIN ESTIMATION METHODS |
ICAS2012-11.9.ST |
| Yuan, W. |
NUMERICAL SIMULATIONS OF
SELF-SUSTAINED AEROELASTIC OSCILLATIONS AT LOW REYNOLDS NUMBERS |
ICAS2012-2.6.3 |
| Yuhara, T. |
CONCEPTUAL DESIGN STUDY ON
LOW BOOM LH2 SUPERSONIC TRANSPORT -
CONSIDERING CLIMATE CHANGE IMPACT |
ICAS2012-1.2.3 |
| Yulong, L. |
THE
NUMERICAL SIMULATION OF BIRD STRIKE ON BLADES OF AN ENGINE |
ICAS2012-4.4.3 |
| Zaichik, L. |
FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS2012-9.3.2 |
| Zaichik, L. E. |
EFFECTS OF MANIPULATOR TYPE
AND FEEL SYSTEM CHARACTERISTICS ON HIGH-FREQUENCY BIODYNAMIC PILOT-AIRCRAFT
INTERACTION |
ICAS2012-5.9.3 |
| Zaichik, L. E. |
SOME ASPECTS OF MOVING-BASE
SIMULATION OF UPSET RECOVERING MANEUVER |
ICAS2012-5.9.4 |
| Zammit-Mangion, D. |
A CASE STUDY OF ARRIVAL AND
DEPARTURE MANAGERS COOPERATION FOR REDUCING AIRBORNE HOLDING TIMES AT
DESTINATION AIRPORTS |
ICAS2012-10.1.ST |
| Zammit-Mangion, D. |
A PROPOSAL FOR REVISED
APPROACHES AND PROCEDURES TO MALTA INTERNATIONAL AIRPORT |
ICAS2012-4.9.3 |
| Zammit-Mangion, D. |
TOWARDS TRAJECTORY
PREDICTION AND OPTIMISATION FOR ENERGY EFFICIENCY OF AN AIRCRAFT WITH
ELECTRICAL AND HYDRAULIC ACTUATION SYSTEMS |
ICAS2012-6.7.3 |
| Zammit-Mangion, D. |
CORRESPONDENCE AND
CLUSTERING METHODS FOR IMAGE-BASED WING-TIP COLLISION AVOIDANCE TECHNIQUES |
ICAS2012-9.10.4 |
| Zammit-Mangion, D. |
BI-OBJECTIVE PSEUDOSPECTRAL
OPTIMAL CONTROL TECHNIQUES FOR AIRCRAFT TRAJECTORY OPTIMIZATION |
ICAS2012-P5.6 |
| Zapotezny-Anderson, P. M. |
DESIGN OF FLIGHT AVOIDANCE
MANOEUVRE ALPHABETS FOR MIXED CENTRALISED-DECENTRALISED SEPARATION MANAGEMENT |
ICAS2012-10.7.3 |
| Zare-Behtash, H. |
PERFORMANCE ANALYSIS OF A
SCRAMJET INLET-ISOLATOR USING EXPERIMENTAL & NUMERICAL METHODS |
ICAS2012-P4.12 |
| Zeng, Z. |
FLEXIBLE WING AERODYNAMICS
AT LOW REYNOLDS NUMBERS |
ICAS2012-3.3.1 |
| Zhang, B. |
FRACTURE
ANALYSIS OF BLADE DOVETAIL OF TC11 TITANIUM ALLOY |
ICAS2012-P4.7 |
| Zhang, J. J. |
THE STUDY ON THE AIRCRAFT
INTEGRATED CHARACTERS WITH DIFFERENT HEIGHT WINGLETS |
ICAS2012-P2.9 |
| Zhang, K. |
LAMINAR FLOW WING’S
OPTIMIZATION DESIGN BY RANS SOLVER WITH AUTOMATIC TRANSITION PREDICTION |
ICAS2012-2.2.3 |
| Zhang, K. -S |
DESIGN OF LAMINAR
SUPERCRITICAL AIRFOILS BASED ON NAVIER-STOKES EQUATIONS |
ICAS2012-2.2.2 |
| Zhang, K. -S. |
MULTIDISCIPLINARY EVALUATION
OF TRUSS-BRACED WING FOR FUTURE GREEN AIRCRAFT |
ICAS2012-1.10.ST |
| Zhang, R. |
THE WORKFLOW CONSTRUCTION
AND MANAGEMENT IN AERONAUTICAL MULTIDISCIPLINARY OPTIMIZATION |
ICAS2012-2.1.2 |
| Zhang, R. |
A GENERAL FOOTPRINT
GENERATION APPROACH FOR LIFTING RE-ENTRY VEHICLE |
ICAS2012-5.7.2 |
| Zhang, R. |
ANGLE OF ATTACK OPERATION
ZONE ANALYSIS AND DESIGN FOR LIFTING ENTRY |
ICAS2012-5.7.3 |
| Zhang, R. |
A NEW APPROACH FOR RE-ENTRY
VEHICLE TRAJECTORY PLANNING AND GUIDANCE |
ICAS2012-5.7.5 |
| Zhang, R. |
THE METHOD FOR NONLINEAR
ANALYSIS OPTIMIZATION IN AERONAUTICAL RESEARCH |
ICAS2012-P1.2 |
| Zhang, S. C. |
LCF BEHAVIOR AND LIFE
EVALUATION OF A SINGLE CRYSTAL NICKEL BASE SUPERALLOY UNDER DIFFERENT DWELL
CONDITION |
ICAS2012-7.3.3 |
| Zhang, T. |
RESEARCH ON CRACK GROWTH OF
MULTIPLE-SITE DAMAGED STRUCTURE |
ICAS2012-7.1.3 |
| Zhang, W. |
RESEARCH ON METHODS OF
DYNAMIC MODELING AND SIMULATION FOR MORPHING WING AIRCRAFT |
ICAS2012-5.10.ST |
| Zhang, W. |
THE GLARE EVALUATION METHOD
FOR CIVIL AIRPLANE FLIGHT DECK |
ICAS2012-9.3.3 |
| Zhang, W. S. |
NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS2012-2.3.3 |
| Zhang, X. |
EXTENSIONS OF MENTER’S SST
TRANSITION MODEL TO SIMULATE HYPERSONIC AND CROSS-FLOW TRANSITION |
ICAS2012-11.4.ST |
| Zhang, X. |
DEVELOPMENT
OF THE OPTIMIZED APPROACH AND LANDING TRAJECTORY FOR FUTURE AIR TRANSPORT
SYSTEM |
ICAS2012-P8.1 |
| Zhang, X. Q. |
THE DYNAMIC BEHAVIOR OF
FUNCTIONALLY GRADED PLATES UNDER THE IMPACT LOADING |
ICAS2012-7.7.3 |
| Zhang, Y. |
NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS2012-2.3.3 |
| Zhang, Z. B. |
THE
INTEGRATION OPTIMIZATION DESIGN OF AERODYNAMIC AND STEALTH FOR FIGHTERS |
ICAS2012-P2.2 |
| Zhang, Z. B. |
EXPERIMENTAL
INVESTIGATION OF INFRARED STEALTH TECHNOLOGIES OF AERO-ENGINE EXHAUST SYSTEM |
ICAS2012-P4.1 |
| Zhang, Z.- H. |
NUMERICAL INVESTIGATION OF
FLOW OVER MULTI-ELEMENT AIRFOILS WITH LIFT-ENHANCING TABS |
ICAS2012-2.3.2 |
| Zhao, K. |
CFD-BASED RESEARCH OF STRAKE
EFFECTS FOR LOW SPEED HIGH LIFT CONFIGURATION |
ICAS2012-P2.16 |
| Zhao, K. |
NUMERICAL SIMULATION OF
TRANSONIC SHOCK-VORTEX INTERACTION FLOW AROUND THE VFE-2 DELTA WING BASED ON
MDDES |
ICAS2012-P2.4 |
| Zhao, N. |
NUMERICAL
SIMULATION OF BIRD-STRIKING PROCESS AND ITS EXPERIMENTAL VERIFICATION |
ICAS2012-8.9.4 |
| Zhao, W. |
STUDIES ON IMPROVEMENT OF
NONLINEAR PITCHING MOMENT CHARACTERISTICS OF CRANKED-ARROW WING |
ICAS2012-3.2.1 |
| Zhao, Y. |
STUDY ON THE FLOW STRUCTURES
OF THE SHOCKWAVE AND TURBULENT BOUNDARY-LAYER INTERACTION |
ICAS2012-11.4.3 |
| Zheng, X. |
ON
THE KNEE-POINT PHENOMENON IN COMPOSITE LAMINATES UNDER LOW-VELOCITY IMPACT
AND QUASI-STATIC INDENTATION |
ICAS2012-7.7.ST |
| Zhong, B. |
EXTENSIONS OF MENTER’S SST
TRANSITION MODEL TO SIMULATE HYPERSONIC AND CROSS-FLOW TRANSITION |
ICAS2012-11.4.ST |
| Zhong, Y. |
CFD-BASED RESEARCH OF STRAKE
EFFECTS FOR LOW SPEED HIGH LIFT CONFIGURATION |
ICAS2012-P2.16 |
| Zhou, H. |
DEVELOPMENT
OF THE OPTIMIZED APPROACH AND LANDING TRAJECTORY FOR FUTURE AIR TRANSPORT
SYSTEM |
ICAS2012-P8.1 |
| Zhou, T. |
NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS2012-2.3.3 |
| Zhu, J. |
APPLICATION
OF TWO TRANSITION MODELS TO FLOWS AROUND AIRFOILS |
ICAS2012-2.4.4 |
| Zhu, J. J. |
THE PERFORMANCE COMPUTATION
OF THE HOT AIR ANTI-ICING SYSTEM OF AN AERO-ENGINE CONE |
ICAS2012-2.6.2 |
| Zhu, K. H. |
THE GENERALIZED ARRIVAL
PLANNER (GARP): MODELING AND ANALYSIS FOR ARRIVAL PLANNING |
ICAS2012-10.9.3 |
| Zhu, Y. |
ANALYZING AND MODELING OF
JAMMING DESTROY FACTOR |
ICAS2012-P6.1 |
| Zhu, Z. |
LAMINAR FLOW WING’S
OPTIMIZATION DESIGN BY RANS SOLVER WITH AUTOMATIC TRANSITION PREDICTION |
ICAS2012-2.2.3 |
| Zhuang, Q. |
EFFECT ON THE AERODYNAMIC
FORCING IN AN AXIAL TURBINE STAGE ON VARYING STATOR BLADE SHAPE |
ICAS2012-4.3.ST |
| Zichenkov, M. |
ANALYSIS OF STATIC AND
DYNAMIC AEROELASTIC CHARACTERISTICS OF AIRPLANE IN TRANSONIC FLOW |
ICAS2012-8.10.4 |
| Zietarski, S. |
A NEW APPROACH TO IDENTIFICATION AND OPTIMIZATION OF AIRFOILS
BY USING THE COMBINATORIAL-CYCLIC METHOD |
ICAS2012-P2.24 |
| Zoltak, J. |
OPTIMISATION OF THE
HELICOPTER FUSELAGE WITH SIMULATION OF MAIN AND TAIL ROTOR INFLUENCE |
ICAS2012-1.4.1 |
|
|
|