| Name |
Title |
ICAS Paper Number |
| Abbot, T. S. |
SIMULATION RESULTS FOR AIRBORNE PRECISION SPACING ALONG CONTINUOUS DESCENT ARRIVALS |
ICAS 2008-11.9.2 (AIAA 2008-8931) |
| Abdalla, A. M. |
AERO-STRUCTURAL MDO OF A SPAR-TANK-TYPE WING FOR AIRCRAFT CONCEPTUAL DESIGN |
ICAS2008-1.1 ST: |
| Abdi, F. |
COHESIVE DISINTEGRATION IN IMPACTED RE-ENTRY SPACE TRANSPORTATION HYBRID STRUCTURES |
ICAS 2008-7.5.1 |
| Abdi, F. |
PREDICTION OF DELAMINATION IN ADVANCED AEROSPACE COMPOSITE STRUCTURES USING MICRO/MACRO MECHANICS CONSTITUTIVE METHODS |
ICAS 2008-7.5.3 |
| Abedian, A. |
AN ANALYTICAL MODEL FOR PREDICTION OF THE STEADY STATE CREEP DEFORMATIONS AND STRESSES OF SHORT FIBER COMPOSITES |
ICAS 2008-9.8.3 |
| Abedian, A. |
EFFECTS OF HIERARCHY ORDER ON NATURAL FREQUENCY AND VIBRATION TRANSMISSION OF SELF-SIMILAR TRUSSES |
ICAS2008-P3.9 |
| Abedian, A. |
FEM MICRO-MECHANICAL ANALYSIS OF DELAMINATION PHENOMENON IN IMC LAMINATED COMPOSITES USING DAMAGE THEORY |
ICAS2008-9.4 ST: |
| Abedian, A. |
MICROMECHANICAL FEM MODELING OF THERMAL STRESSES IN FUNCTIONALLY GRADED MATERIALS |
ICAS 2008-7.2.4 |
| Abedian, A. |
MULTIDISCIPLINARY DESIGN OPTIMIZATION OF A SATELLITE BOOM STRUCTURE TO REDUCE WEIGHT AND VIBRATION TRANSMISSION USING GA |
ICAS2008-P3.8 |
| Abrahamson, P. D. |
DEVELOPMENT AND APPLICATION OF AN INTEGRATED APPROACH TOWARD NASA AIRSPACE SYSTEMS RESEARCH |
ICAS 2008-10.8.1 (AIAA 2008-8924) |
| Adams, N. A. |
AERODYNAMIC INVESTIGATIONS ON A GENERIC FAN-IN-WING CONFIGURATION |
ICAS 2008-3.5.1 |
| Adeyefa, S. |
EVAPORATING COOLANT FOR ON-BOARD COOLING SYSTEMS WITH DIRECT CONDENSATION THROUGH AMBIENT AIR |
ICAS 2008-6.6.3 |
| Adzic, M. |
ON AIRCRAFT PERFORMANCE IMPROVEMENT BY USING WINGLETS |
ICAS 2008-2.8.3 |
| Ahmad, N. |
AIRSHIP TRANSPORT OPERATIONAL MANAGEMENT IN NORTHERN LATITUDES |
ICAS 2008-10.1.1 (AIAA 2008-8850) |
| Airoldi, A. |
DESIGN AND MANUFACTURING OF COMPOSITE CHIRAL STRUCTURES WITH MORPHING CAPABILITIES |
ICAS 2008-7.8.1 |
| Akbarpour, S. |
MICROMECHANICAL FEM MODELING OF THERMAL STRESSES IN FUNCTIONALLY GRADED MATERIALS |
ICAS 2008-7.2.4 |
| Alderliesten, R. C. |
FATIGUE CRACK GROWTH PREDICTION OF FIBRE REINFORCED METAL LAMINATES UNDER VARIABLE AMPLITUDE LOADING |
ICAS 2008-7.6.1 |
| Alderliesten, R. C. |
THE INFLUENCE OF FATIGUE CRACK INITIATION BEHAVIOUR OF FRICTION STIR WELDED JOINTS ON THE DESIGN CRITERIA |
ICAS 2008-7.6.2 |
| Allen, C. B. |
TOWARDS AERODYNAMIC OPTIMISATION OF AN AEROELASTIC WING USING DOMAIN ELEMENT PARAMETERISATION |
ICAS 2008-2.8.1 |
| Allen, D. |
HEALTH MONITORING FOR COMMERCIAL AIRCRAFT SYSTEMS |
ICAS 2008-6.1.2 |
| Allerton, D. J. |
REAL-TIME SIMULATION OF A DISTRIBUTED CONFLICT RESOLUTION ALGORITHM |
ICAS 2008-8.7.3 |
| Alves, P. M. |
AVIATION TELEMEDICINE: PAST, PRESENT AND FUTURE |
ICAS 2008-9.2.2 |
| Amadori, K. |
AIRCRAFT CONCEPTUAL DESIGN AUTOMATION |
ICAS 2008-1.8.1 |
| Amadori, K. |
RAVEN – A SUBSCALE RADIO CONTROLLED BUSINESS JET DEMONSTRATOR |
ICAS 2008-5.5.2 |
| Amelsberg, S. |
AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION FOR TAKE-OFF AND DEPARTURE |
ICAS 2008-11.8.3 (AIAA 2008-8921) |
| Amelsberg, S. |
GENERATION OF HIGH ACCURATE 4D TRAJECTORIES FOR TAKE-OFF AND DEPARTURE |
ICAS2008-8.11 ST: |
| Amiryants, G. |
ACTIVE AEROELASTICITY CONCEPT: NOVEL VIEW, METHODOLOGY AND RESULTS |
ICAS 2008-9.6.1 INVITED |
| An, G. |
THE NUMERICAL SIMULATION ANALYSIS OF KEY STRUCTURES OF INTEGRATED POWER SUPPLY IN MOTOR-PUMP |
ICAS2008-P6.2 |
| An, S. J. |
UNSTEADY PROPULSIVE CHARACTERISTICS OF BIOFOILS MOVING IN A VERY LOW-REYNOLDS NUMBER FLOW |
ICAS 2008-3.9.3 |
| An, W. G. |
A NEW EFFICIENT INTERACTIVE MULTI-OBJECTIVE EVOLUTIONARY OPTIMIZATION ALGORITHM AND APPLICATION IN ENGINEERING |
ICAS2008-6.2 ST: |
| Anand, V. |
APPLICATION OF SHAPE OPTIMISATION TO AIRCRAFT WING STRUCTURES |
ICAS 2008-7.8.3 |
| Anastasijevic, Z. |
APPLICATION OF SEMICONDUCTOR STRAIN GAUGES IN MEASUREMENTS OF DYNAMIC STABILITY DERIVATIVES IN THE T-38 WIND TUNNEL |
ICAS 2008-3.4.5 |
| Andersson, H. |
HOSTED SIMULATION FOR HETEROGENEOUS AIRCRAFT SYSTEM DEVELOPMENT |
ICAS2008-6.2 ST: |
| Ando, T. |
DEVELOPMENT OF AN ONBOARD DOPPLER LIDAR FOR FLIGHT SAFETY |
ICAS 2008-9.9.2 |
| Anghileri, M. |
BIRDSTRIKE ONTO STRUCTURES IN ROTATIONAL MOTION |
ICAS 2008-9.4.4 |
| Anghileri, M. |
SURVEY OF FEASIBLE NUMERICAL APPROACHES TO ANALYSE THE BEHAVIOUR OF A COMPOSITE SKIN PANEL DURING A WATER IMPACT |
ICAS 2008-7.9.2 |
| Antunes, A. P. |
AN AERODYNAMIC OPTIMIZATION FRAMEWORK BASED ON GENETIC ALGORITHMS |
ICAS 2008-2.3.4 |
| Aoki, T. |
IMPACT CHARACTERISTICS ESTIMATION OF SHORT SUPPORT COLUMNS UNDER CABIN FLOOR |
ICAS 2008-9.4.1 |
| Arendsen, P. |
OPTIMISING HIGH-EFFICIENCY RUDDERS FOR TRANSPORT AIRCRAFT FUEL BURN REDUCTION |
ICAS 2008-2.11.2 |
| Arimoto, M. |
DEVELOPMENT OF THE DISPLAY DEVICE OF POWER DISTIBUTION SYSTEM (DEVELOPMENT OF THE DEPTH FUSED 3-D DISPLAY FOR AIRCRAFT) |
ICAS2008-6.5 ST: |
| Arizono, H. |
TRANSONIC FLUTTER WIND TUNNEL TESTS OF CONVENTIONAL TWIN-ENGINE TRANSPORT SEMISPAN MODEL |
ICAS 2008-9.6.2 |
| Armstrong, M. |
FUNCTION BASED ARCHITECTURE DESIGN SPACE DEFINITION AND EXPLORATION |
ICAS 2008-1.9.3 (AIAA 2008-8928) |
| Armstrong, M. |
METHODOLOGY FOR AIRCRAFT SYSTEM ARCHITECTURE SIZING |
ICAS 2008-6.2.2 |
| Asai, K. |
EXPERIMENTAL STUDY ON INTERFERENCE FLOW OF A SUPERSONIC BUSEMANN BIPLANE USING PRESSURE-SENSITIVE PAINT TECHNIQUE |
ICAS 2008-3.7.5 |
| Aschenbrenner, L. |
MECHANICS OF COMPOSITES IN LIGHTWEIGHT STRUCTURES: EFFICIENT TESTING AND COMPUTATION ACCOUNTING FOR COMPLEX 3D BEHAVIOUR |
ICAS 2008-7.11.2 |
| Asim, M. |
FRAMEWORK OF PAKISTAN AEROSPACE INDUSTRY QUALITY SYSTEM |
ICAS 2008-6.9.4 |
| Aso, S. |
AERODYNAMIC DESIGN AND ITS VALIDATION OF AN OPEN-TYPE ENGINE RUN-UP FACILITY |
ICAS 2008-4.5.3 |
| Aso, S. |
CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION |
ICAS 2008-1.2.3 |
| Aso, S. |
NUMERICAL STUDY OF THE EFFECT OF THE OPPOSING JET ON REDUCTION OF AERODYNAMIC HEATING WITH DIFFERENT NOSE CONFIGURATIONS |
ICAS 2008-3.6.3 |
| Astarita, T. |
EXPERIMENTAL ANALYSIS OF THE FLOW FIELD IN A ROTATING 'U' CHANNEL |
ICAS 2008-4.6.3 |
| Astarita, T. |
MODULATION TRANSFER FUNCTION OF STEREO PARTICLE IMAGE VELOCIMETRY TECHNIQUE |
ICAS2008-P2.6 |
| Atkins, S. |
IMPLICATION OF VARIABILITY IN AIRPORT SURFACE OPERATIONS ON 4-D TRAJECTORY PLANNING |
ICAS 2008-11.11.3 (AIAA 2008-8960) |
| Atkins, S. |
IMPROVED PREDICTION OF GATE DEPARTURE TIMES USING PRE-DEPARTURE EVENTS |
ICAS 2008-11.8.1 (AIAA 2008-8919) |
| Atobe, T. |
LARGE EDDY SIMULATION AROUND 2-D AIRFOIL WITH NATURAL TRANSITION AT HIGH REYNOLDS NUMBERS |
ICAS2008-2.1 ST: |
| Attia, M. S. |
APPLICATION OF THE INTEGRATED PRODUCT TEAM (IPT) CONCEPT TO THE RE-ENGINE OF A VERY LIGHT JET (VLJ) |
ICAS 2008-6.7.5 |
| Auger, D. |
FLIGHT SIMULATORS – ON DIFFERENT PERCEPTIONS OF MANUFACTURERS, AVIATION AUTHORITIES, RESEARCH AND USERS |
ICAS 2008-5.5.1 INVITED |
| Auriti, L. |
CESSNA CITATION CJ1 FLIGHT TEST DATA GATHERING AND LEVEL-C SIMULATOR MODEL DEVELOPMENT |
ICAS 2008-5.1.2 |
| Aversa, N |
MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
| Axelsson, L.-U. |
EVALUATION OF THE FLOW IN AN INTERMEDIATE TURBINE DUCT AT OFF-DESIGN CONDITIONS |
ICAS 2008-4.6.2 |
| Ayuso, L. |
AERODYNAMIC OPTIMIZATION OF A BLENDED WING BODY |
ICAS2008-2.11 ST: |
| Azevedo, J. L. F. |
AN AERODYNAMIC OPTIMIZATION FRAMEWORK BASED ON GENETIC ALGORITHMS |
ICAS 2008-2.3.4 |
| Azevedo, J. L. F. |
APPLICATION OF A NAVIER-STOKES CODE TO THE SIMULATIONS OF HIGH-LIFT DEVICES USING UNSTRUCTURED GRIDS |
ICAS 2008-2.2.4 |
| Azevedo, J. L. F. |
DYNAMIC ANALYSIS OF AEROELASTIC RESPONSE FOR TRANSONIC FLOW WITH NONLINEAR STRUCTURAL MODEL |
ICAS 2008-9.6.4 |
| Badalamenti, C. |
VORTEX SHEDDING FROM A ROTATING CIRCULAR CYLINDER AT MODERATE SUB-CRITICAL REYNOLDS NUMBERS AND HIGH VELOCITY RATIO |
ICAS 2008-3.10.5 |
| Badanik, B. |
AIRLINES’ POINT OF VIEW AS A NEW APPROACH TO MEASURING QUALITY OF SERVICE AT AIRPORTS |
ICAS 2008-8.3.3 |
| Badiey, M. |
MULTIDISCIPLINARY DESIGN OPTIMIZATION OF A SATELLITE BOOM STRUCTURE TO REDUCE WEIGHT AND VIBRATION TRANSMISSION USING GA |
ICAS2008-P3.8 |
| Bagassi, S. |
DESIGN AND DEVELOPMENT OF AN ATC DISTRIBUTED TRAINING SYSTEM |
ICAS2008-P8.2 (AIAA 2008-8873) |
| Bagassi, S. |
DESIGN AND EVALUATION OF A 4D INTERFACE FOR ATC |
ICAS 2008-9.10.3 |
| Bai, J. |
SATELLITE-BASED NAVIGATION ARCHITECTURE STUDY FOR AIRCRAFT CATEGORY III LANDINGS |
ICAS 2008-6.4.4 |
| Bailey, L. |
TAILORED ARRIVALS OPERATIONS AT SFO AND EXPECTED ENVIRONMENTAL BENEFITS |
ICAS 2008-11.3.4 (AIAA 2008-8868) |
| Baklanov, V. |
PROBLEMS OF VIBROACOUSTICS FOR NEW AIRPLANE GENERATION |
ICAS 2008-4.9.4 |
| Balasubramanian, S. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
| Baldomir, A. |
SIZE OPTIMIZATION OF AIRCRAFT STRUCTURES |
ICAS2008-7.11 ST: |
| Baldwin, K. |
AN AUTOMATED SIMULATION PILOT CAPABILITY TO SUPPORT ADVANCED AIR TRAFFIC CONTROLLER TRAINING |
ICAS 2008-10.5.3 (AIAA 2008-8897) |
| Balzer, W. |
INVESTIGATION OF SEPARATION CONTROL FOR LOW-PRESSURE TURBINES USING CFD |
ICAS 2008-4.4.2 |
| Banerjee, S. |
LOW COST TRANS-RIVER AERIAL-FERRY USING A NOVEL LTA SYSTEM |
ICAS 2008-10.1.2 (AIAA 2008-8851) |
| Bansmer, S. |
A COMPARISON OF NUMERICAL RANS SIMULATIONS AND FLOW FIELD MEASUREMENTS OF AN OSCILLATING AIRFOIL FOR FLAPPING WING PROPULSION |
ICAS 2008-2.10.2 |
| Barhydt, R. |
DEVELOPMENT AND APPLICATION OF AN INTEGRATED APPROACH TOWARD NASA AIRSPACE SYSTEMS RESEARCH |
ICAS 2008-10.8.1 (AIAA 2008-8924) |
| Barmore, B. E. |
SIMULATION RESULTS FOR AIRBORNE PRECISION SPACING ALONG CONTINUOUS DESCENT ARRIVALS |
ICAS 2008-11.9.2 (AIAA 2008-8931) |
| Barret et al, S. |
INTERDEPENDENCIES IN LOCAL AIR QUALITY AND NOISE IMPACTS FOR LANDING AND TAKEOFF OPERATIONS |
ICAS 2008-11.3.2 (AIAA 2008-8866) |
| Barrett, T. |
THE QUEST FOR A TRULY PARSIMONIOUS AIRFOIL PARAMETERIZATION SCHEME |
ICAS2008-P2.2 (AIAA 2008-8879) |
| Barros, P. A. |
AN APPROACH FOR VERIFICATION AND VALIDATION OF THE ENVIRONMENTAL DESIGN SPACE |
ICAS2008-P8.4 (AIAA 2008-8875) |
| Basso, E. |
APPLICATION OF A NAVIER-STOKES CODE TO THE SIMULATIONS OF HIGH-LIFT DEVICES USING UNSTRUCTURED GRIDS |
ICAS 2008-2.2.4 |
| Basso, N. |
INVESTIGATION OF ADHESIVELY BONDED COMPOSITE STRUCTURE JOINTS |
ICAS 2008-7.2.1 |
| Bateman, H. L. |
SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
| Battezzato, A. |
FLY-BY-WIRE CONTROL OF A HELICOPTER: MULTIBODY MAIN ROTOR MODEL |
ICAS2008-5.11 ST: |
| Battiste, V. |
ASSESSMENT OF FLIGHT CREW ACCEPTANCE OF AUTOMATED RESOLUTION SUGGESTIONS AND MANUAL RESOLUTION TOOLS |
ICAS 2008-8.7.2 |
| Baumeister, R. |
REAL-TIME SIMULATION OF A DISTRIBUTED CONFLICT RESOLUTION ALGORITHM |
ICAS 2008-8.7.3 |
| Bauschat, J.-M. |
FLIGHT SIMULATORS – ON DIFFERENT PERCEPTIONS OF MANUFACTURERS, AVIATION AUTHORITIES, RESEARCH AND USERS |
ICAS 2008-5.5.1 INVITED |
| Baxley, B. T. |
SIMULATION RESULTS FOR AIRBORNE PRECISION SPACING ALONG CONTINUOUS DESCENT ARRIVALS |
ICAS 2008-11.9.2 (AIAA 2008-8931) |
| Bayandor, J. |
BWB MILITARY CARGO TRANSPORT FUSELAGE DESIGN AND ANALYSIS |
ICAS 2008-7.9.3 |
| Bayandor, J. |
COHESIVE DISINTEGRATION IN IMPACTED RE-ENTRY SPACE TRANSPORTATION HYBRID STRUCTURES |
ICAS 2008-7.5.1 |
| Bayandor, J. |
INVESTIGATION OF ADHESIVELY BONDED COMPOSITE STRUCTURE JOINTS |
ICAS 2008-7.2.1 |
| Bayandor, J. |
PREDICTION OF DELAMINATION IN ADVANCED AEROSPACE COMPOSITE STRUCTURES USING MICRO/MACRO MECHANICS CONSTITUTIVE METHODS |
ICAS 2008-7.5.3 |
| Bayandor, J. |
THE DESIGN OF POSTBUCKLING COMPOSITE AEROSPACE STRUCTURES ACCOUNTING FOR DAMAGE INITIATION AND GROWTH |
ICAS 2008-7.3.2 |
| Bazso, Z. |
CAPACITY RESEARCH OF BRNO-TURANY AIRPORT WITH RESPECT TO NEW TRENDS IN AIR TRANSPORT |
ICAS 2008-8.5.3 |
| Beaton, E. |
INTEGRATED TIME-BASED FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.10.1 (AIAA 2008-8940) |
| Beaumier, P. |
AERODYNAMIC AND AERO-ACOUSTIC DESIGN OF MODERN TILT-ROTORS: THE ONERA EXPERIENCE |
ICAS 2008-1.7.4 |
| Beccaro, A. |
A NEW AIRCRAFT CONCEPT: THE COMBAT MALE |
ICAS 2008-1.4.4 |
| Becker (retired), J. |
APPLICATION OF PVDF FOILS FOR THE MEASUREMENTS OF UNSTEADY PRESSURES ON WIND TUNNEL MODELS FOR THE PREDICTION OF AIRCRAFT VIBRATIONS |
ICAS 2008-3.4.2 |
| Becker, G. G. |
A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
| Becker, H. |
PERFORMANCE-BASED TMA HANDLING FOR MIXED TRAFFIC USING A GROUND BASED 4D-GUIDANCE FOR UNEQUIPPED AIRCRAFT |
ICAS 2008-10.8.3 |
| Beelaerts van Blokland, W. W. A. |
DESIGN OF A LEAN MRO BUSINESS PROCESS FOR EPCOR |
ICAS 2008-10.3.4 (AIAA 2008-8864) |
| Benedictus, R. |
FATIGUE CRACK GROWTH PREDICTION OF FIBRE REINFORCED METAL LAMINATES UNDER VARIABLE AMPLITUDE LOADING |
ICAS 2008-7.6.1 |
| Benedictus, R. |
THE INFLUENCE OF FATIGUE CRACK INITIATION BEHAVIOUR OF FRICTION STIR WELDED JOINTS ON THE DESIGN CRITERIA |
ICAS 2008-7.6.2 |
| Benmeddour, A. |
TARGETING PODS EFFECTS ON STORE SEPARATION CHARACTERISTICS: A JOINT NRC-IAR/USNAVY CFD EFFORT |
ICAS 2008-2.9.2 |
| Bérard, A. |
CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
| Bérard, A. |
DEVELOPMENT AND VALIDATION OF A NEXT-GENERATION CONCEPTUAL AERO-STRUCTURAL SIZING SUITE |
ICAS 2008-1.6.2 |
| Berard, C. |
MODELLING OF THE 3-DOF NONLINEAR AIRCRAFT BEHAVIOUR VIA SMALL STANDARD FORMS |
ICAS2008-P5.5 |
| Berends, J. P. T. J. |
MDO DESIGN SUPPORT BY INTEGRATED ENGINEERING SERVICES WITHIN A MULTI-AGENT TASK ENVIRONMENT |
ICAS 2008-1.11.1 (AIAA 2008-8947) |
| Berezin, A. V. |
ESTIMATION OF CRACK TURN PHENOMENON |
ICAS 2008-7.6.3 |
| Berge et al, M. |
COLLABORATIVE FLOW MANAGEMENT: ANALYSIS OF BENEFITS DURING CONVECTIVE WEATHER DISRUPTIONS |
ICAS 2008-11.7.5 (AIAA 2008-8911) |
| Berge, M. |
ANALYSIS OF ARRIVAL MANAGEMENT PERFORMANCE WITH AIRCRAFT REQUIRED TIME OF ARRIVAL CAPABILITIES |
ICAS 2008-11.9.3 (AIAA 2008-8932) |
| Bergsma, O. K. |
CARBON/DYNEEMA INTRALAMINAR HYBRIDS: NEW STRATEGY TO INCREASE IMPACT RESISTANCE OR DECREASE MASS OF CARBON FIBER COMPOSITES |
ICAS 2008-7.3.4 |
| Berth, C. |
RESEARCH ON INTEGRATED COLLIMATED COCKPIT VISUAL AND FLIGHT INFORMATION SYSTEM |
ICAS 2008-9.10.1 |
| Bertini, F. |
EULER INVERSE THROUGHFLOW MODEL BASED ON AN IMPLICIT UPWIND TIME MARCHING TECHNIQUE |
ICAS 2008-2.3.2 |
| Berton, B. |
A NOVEL RECIPROCAL SOUND TRANSMISSION MEASURING METHOD, APPLIED ON A COMPOSITE FUSELAGE |
ICAS 2008-4.9.3 |
| Bes, C. |
CAPACITY MODELLING FOR FUTURE AERONAUTICAL SAFETY COMMUNICATIONS OVER WIDE AREAS |
ICAS 2008-8.8.2 (AIAA 2008-8952) |
| Bettini, P. |
DESIGN AND MANUFACTURING OF COMPOSITE CHIRAL STRUCTURES WITH MORPHING CAPABILITIES |
ICAS 2008-7.8.1 |
| Beyers, M. E. |
COMPUTATIONAL FLUID DYNAMICS AND EXPERIMENTAL INVESTIGATION OF AIRPLANE STALL DYNAMICS WITH WING CONTAMINATION |
ICAS 2008-3.5.2 |
| Bhadra, D. |
IMPACT OF US-EU OPEN AREA AVIATION TREATY ON US AVIATION: A PARAMETRIC ANALYSIS WITH SIMULATION |
ICAS 2008-10.10.3 (AIAA 2008-8937) |
| Bhatti, J. |
AN EXPERIMENTAL AND COMPUTATIONAL COMPARISON OF THE LOW SPEED AERODYNAMICS OF SQUARE AND CIRCULAR SECTIONED BODIES |
ICAS2008-3.5 ST: |
| Bil, C. |
AN ADAPTABLE METHODOLOGY FOR AUTOMATION APPLICATION DEVELOPMENT |
ICAS 2008-6.2.3 |
| Bil, C. |
APPLICATION OF SHAPE OPTIMISATION TO AIRCRAFT WING STRUCTURES |
ICAS 2008-7.8.3 |
| Bil, C. |
BWB MILITARY CARGO TRANSPORT FUSELAGE DESIGN AND ANALYSIS |
ICAS 2008-7.9.3 |
| Bil, C. |
GENETIC FUZZY CONTROL FOR AUTONOMOUS DUCTED-FAN VTOL UAV |
ICAS 2008-5.9.3 |
| Bil, C. |
KNOWLEDGE MANAGEMENT FOR THROUGH LIFE SUPPORT |
ICAS 2008-6.11.3 |
| Biltgen, P. T. |
PARAMETRIC SYSTEM EFFECTIVENESS ANALYSIS USING ARTIFICIAL NEURAL NETWORKS FOR BATTLE MANAGEMENT |
ICAS 2008-1.3.3 |
| Biltgen, P. T. |
UNCERTAINTY QUANTIFICATION FOR CAPABILITY-BASED SYSTEMS-OF-SYSTEMS DESIGN |
ICAS 2008-1.8.3 |
| Birindelli, M. |
ALTERNATIVE ENERGY BASED SYSTEMS FOR ADVANCED U.A.V.; THE “SAVE” PROJECT |
ICAS2008-6.6 ST: |
| Bisagni, C. |
INVESTIGATION OF ADHESIVELY BONDED COMPOSITE STRUCTURE JOINTS |
ICAS 2008-7.2.1 |
| Bisagni, C. |
METAMODELS FOR THE OPTIMIZATION OF DAMAGE-TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.3.3 |
| Blake, W. |
SUPERSONIC AIRCRAFT FORMATION FLYING TO INCREASE FLIGHT EFFICIENCY |
ICAS 2008-1.10.2 |
| Böck, P. |
IMPACT OF ESTOL CAPABILITY ON RUNWAY CAPACITY - AN ANALYTICAL APPROACH |
ICAS 2008-11.9.4 (AIAA 2008-8933) |
| Bock, S. |
"ACTIVE CORE" - A KEY TECHNOLOGY FOR MORE ENVIRONMENTALLY FRIENDLY AERO ENGINES BEING INVESTIGATED UNDER THE NEWAC PROGRAM |
ICAS 2008-4.2.1 |
| Boillot, A. |
FROM BEAM MODELS TO GLOBAL 3D MODELS FOR ROBUST LANDING GEAR DESIGN |
ICAS2008-7.11 ST: |
| Bolczak, C. N. |
SECURE AIRSPACE: A CRITICAL COMPONENT OF NEXTGEN'S LAYERED, ADAPTIVE SECURITY |
ICAS 2008-11.5.2 (AIAA 2008-8893) |
| Bombardi, T. |
3D OBSTACLE AVOIDANCE STRATEGIES FOR UAS (UNINHABITED AERIAL SYSTEMS) MISSION PLANNING AND RE-PLANNING |
ICAS 2008-5.6.1 (AIAA 2008-8962) |
| Bonazountas, M. |
92 LANDING-AVIONIC SYSTEM FOR SMALL-MEDIUM AIRCRAFT FOR AUTOMATED LANDING ON SMALL-MEDIUM AND/OR POORLY EQUIPPED AIRPORTS |
ICAS2008-P6.8 |
| Bone, R. |
SAY WHO? PILOTED SIMULATION STUDY OF COMMUNICATIONS CENTERED AROUND A COCKPIT TRAFFIC DISPLAY |
ICAS 2008-10.5.1 (AIAA 2008-8895) |
| Bonn, J. |
THE MODERNIZED NATIONAL AIRSPACE SYSTEM PERFORMANCE ANALYSIS CAPABILITY (NASPAC) |
ICAS 2008-9.11.2 (AIAA 2008-8945) |
| Bosbach, J. |
SCALING OF MIXED CONVECTION IN AIRCRAFT CABINS |
ICAS 2008-6.3.3 |
| Botin, A. V. |
NUMERICAL AND EXPERIMENTAL STUDIES OF SHOCK INTERFERENCE IN HYPERSONIC FLOWS NEAR A CYLINDER |
ICAS2008-P2.3 |
| Bourdiaudhy, K. |
A FLIGHT THRUST DECK FOR THE F100 TURBOFAN OF THE F16 AIRCRAFT |
ICAS 2008-4.5.1 |
| Bouwmeester, J. G. H. |
CARBON/DYNEEMA INTRALAMINAR HYBRIDS: NEW STRATEGY TO INCREASE IMPACT RESISTANCE OR DECREASE MASS OF CARBON FIBER COMPOSITES |
ICAS 2008-7.3.4 |
| Bower, G. C. |
MULTI-OBJECTIVE AIRCRAFT OPTIMIZATION FOR MINIMUM COST AND EMISSIONS OVER SPECIFIC ROUTE NETWORKS |
ICAS 2008-10.6.3 (AIAA 2008-8905) |
| Brandin, J. |
A STUDY OF AN USER AND ENVIRONMENTAL FRIENDLY STORED ENERGY BASED EPU/APU-SYSTEM FOR MILITARY AEROSPACE APPLICATIONS |
ICAS 2008-6.4.5 |
| Brandt, S. |
ASSESSMENT OF FLIGHT CREW ACCEPTANCE OF AUTOMATED RESOLUTION SUGGESTIONS AND MANUAL RESOLUTION TOOLS |
ICAS 2008-8.7.2 |
| Braun, M. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
| Breeman, J. |
A SIMULATION BENCHMARK FOR AIRCRAFT SURVIVABILITY ASSESSMENT |
ICAS 2008-9.3.2 |
| Breitsamter, C. |
AERODYNAMIC INVESTIGATIONS ON A GENERIC FAN-IN-WING CONFIGURATION |
ICAS 2008-3.5.1 |
| Breitsamter, C. |
FIN BUFFET CHARACTERISTICS OF ADVANCED TRAINER AIRCRAFT |
ICAS 2008-3.4.1 |
| Brezillon, J. |
NUMERICAL AERODYNAMIC OPTIMISATIONS OF 3D HIGH-LIFT CONFIGURATIONS |
ICAS 2008-2.2.3 |
| Brinton, C. |
IMPLICATION OF VARIABILITY IN AIRPORT SURFACE OPERATIONS ON 4-D TRAJECTORY PLANNING |
ICAS 2008-11.11.3 (AIAA 2008-8960) |
| Brinton, C. |
MICROSCOPIC ANALYSIS OF AIRPORT SURFACE SEQUENCING |
ICAS2008-11.11 ST (AIAA 2008-8961) |
| Broichhausen, K. |
A NEW APPROACH FOR CO2 REDUCTION APPLYING STATE-OF-THE-ART ENGINE AND AIRFRAME TECHNOLOGY |
ICAS2008-4.2 ST (AIAA 2008-8974) |
| Broichhausen, K. |
POTENTIALS OF LIGHTER-THAN-AIR TECHNOLOGY IN FUTURE MARKETS – AN EVALUATION |
ICAS2008-P1.7 |
| Broichhausen, K. |
PROMISING FUTURE AIRCRAFT CONCEPT – ESTOL |
ICAS2008-P1.8 |
| Broncheau, J. W. |
SIMULATION OF A NON-AXISYMMETRIC UNDERSEA VEHICLE USING A RECURSIVE NEURAL NETWORK |
ICAS 2008-5.8.2 |
| Brown, A. P. |
COMPUTATIONAL FLUID DYNAMICS AND EXPERIMENTAL INVESTIGATION OF AIRPLANE STALL DYNAMICS WITH WING CONTAMINATION |
ICAS 2008-3.5.2 |
| Brown, N. |
GOING GREEN – MITIGATING AVIATION’S NEW ENVIRONMENTAL DRIVERS |
ICAS 2008-4.7.2 |
| Brown, N. |
THE FEASIBILITY AND POTENTIAL ENVIRONMENTAL BENEFITS OF ALTERNATIVE FUELS FOR COMMERCIAL AVIATION |
ICAS 2008-4.7.5 |
| Brunet, M. |
A NOVEL APPROACH TO AIR TRANSPORT SYSTEM ENVIRONMENTAL IMPACT EVALUATION THROUGH PHYSICAL MODELLING AND SIMULATION |
ICAS2008-8.3 ST: |
| Bublitsky, B. |
INNOVATIVE APPROACH FOR FUTURE AIRCRAFT DEVELOPMENT AT IAI |
ICAS 2008-1.6.1 |
| Bucher, B. |
UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
| Bueno, J. |
SAFE AUTOMATIC FLIGHT BACK AND LANDING OF AIRCRAFT (SOFIA) |
ICAS2008-9.7 ST: |
| Buoni, G. P. |
LARGE UAS OPERATIONS IN THE NAS - THE NASA 2007 WESTERN STATES FIRE MISSIONS |
ICAS 2008-8.1.3 (AIAA 2008-8967) |
| Buonomo, B. |
VORTEX BLOB METHOD AS VISUALIZATION TOOL FOR MULTI-ELEMENT AIRFOIL FLOWS OPTIMIZATION |
ICAS 2008-3.9.2 |
| Burke, R. |
AUTOMATED ASSEMBLY TIME ANALYSIS USING A DIGITAL KNOWLEDGE BASED APPROACH |
ICAS 2008-10.3.1 (AIAA 2008-8861) |
| Burke, R. |
USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
| Burleson, C. |
GOING GREEN – MITIGATING AVIATION’S NEW ENVIRONMENTAL DRIVERS |
ICAS 2008-4.7.2 |
| Bushnell, L. |
SECURITY OF WIRELESS SENSOR NETWORK ENABLED HEALTH MONITORING FOR FUTURE AIRPLANES |
ICAS 2008-9.1.3 |
| Bussink, F. J. L. |
A PERFORMANCE ASSESSMENT OF A TACTICAL AIRBORNE SEPARATION ASSISTANCE SYSTEM USING REALISTIC, COMPLEX TRAFFIC FLOWS |
ICAS 2008-11.4.4 (AIAA 2008-8884) |
| Bussink, F. J. L. |
OPERATIONAL IMPROVEMENTS FROM IN-TRAIL PROCEDURE IN THE NORTH ATLANTIC ORGANIZED TRACK SYSTEM |
ICAS 2008-11.6.1 (AIAA 2008-8898) |
| Bussink, F. J. L. |
PILOT IN-TRAIL PROCEDURE VALIDATION SIMULATION STUDY |
ICAS 2008-10.5.2 (AIAA 2008-8896) |
| Butler, J. D. |
A STUDY OF SHEAR LAYER SUB-STRUCTURES IN LEADING EDGE VORTICES USING LASER DOPPLER VELOCIMETRY |
ICAS 2008-2.1.3 |
| Butterfield, J. |
AUTOMATED ASSEMBLY TIME ANALYSIS USING A DIGITAL KNOWLEDGE BASED APPROACH |
ICAS 2008-10.3.1 (AIAA 2008-8861) |
| Butterfield, J. |
USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
| Byun, Y. -H. |
A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
| Caixeta Jr., P. R. |
AERO-STRUCTURAL MDO OF A SPAR-TANK-TYPE WING FOR AIRCRAFT CONCEPTUAL DESIGN |
ICAS2008-1.1 ST: |
| Calabrò, A. |
AN ORIGINAL SYSTEM TO MEASURE ADAPTIVE STRUCTURE PARAMETERS USING FIBER OPTIC |
ICAS2008-7.4 ST: |
| Callantine, T. |
CONTROLLER SUPPORT FOR MANAGING HIGH-EFFICIENCY ARRIVALS IN DENSE TRAFFIC ENVIRONMENTS |
ICAS 2008-11.10.4 (AIAA 2008-8943) |
| Camilo, E. |
DYNAMIC ANALYSIS OF AEROELASTIC RESPONSE FOR TRANSONIC FLOW WITH NONLINEAR STRUCTURAL MODEL |
ICAS 2008-9.6.4 |
| Campos, L. M. B. C. |
391 EFFECT OF ATMOSPHERIC PROPAGATION ON AIRCRAFT NOISE |
ICAS2008-P10.1 |
| Campos, L. M. B. C. |
ON THE EFFECTS ON NOISE OF GROUND REFLECTION AND ATMOSPHERIC ATTENUATION ON THE NOISE OF HELICOPTERS |
ICAS 2008-3.9.4 |
| Campos, L. M. B. C. |
ON THE MINIMIZATION OF CRUISE DRAG DUE TO PITCH TRIM FOR A FLYING-WING CONFIGURATION |
ICAS 2008-5.3.3 |
| Campos, L. M. B. C. |
ON THE PROBABILITY OF COLLISION FOR CLIMBING AND DESCENDING TRAJECTORIES RELEVANT TO AIR TRAFFIC MANAGEMENT |
ICAS2008-9.3 ST: |
| Campos, N. V. |
PRELIMINARY ANALYSIS OF STRATEGIES AND CHALLENGES TO ENCOURAGE DATA LINK ADOPTION OVER THE NORTH ATLANTIC AIRSPACE |
ICAS 2008-8.8.3 (AIAA 2008-8953) |
| Canders, R. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
| Cannata, M. |
TRANSVERSAL INJECTED SYNTHETIC JETS FOR WALL TURBULENCE CONTROL |
ICAS 2008-3.10.3 |
| Capello, E. |
TRAJECTORY OPTIMISATION FOR AUTONOMOUS VEHICLES: A MINIUAV APPLICATION |
ICAS 2008-5.6.3 |
| Capron, W. R. |
SIMULATION RESULTS FOR AIRBORNE PRECISION SPACING ALONG CONTINUOUS DESCENT ARRIVALS |
ICAS 2008-11.9.2 (AIAA 2008-8931) |
| Carbaugh, D. |
THE SAFETY GAINED BY EQUIPMENT AND PROCEDURES USED TO PERFORM CONSTANT ANGLE APPROACHES |
ICAS 2008-9.7.3 |
| Carl, U. |
EVAPORATING COOLANT FOR ON-BOARD COOLING SYSTEMS WITH DIRECT CONDENSATION THROUGH AMBIENT AIR |
ICAS 2008-6.6.3 |
| Carl, U. |
MULTIVARIABLE CONTROLLER DESIGN FOR A TRIMMABLE HORIZONTAL STABILIZER ACTUATOR WITH TWO PRIMARY LOAD PATHS |
ICAS 2008-6.4.2 |
| Carl, U. B. |
MONITORING OF OSCILLATORY FAILURE CASES FOR THE REDUCTION OF STRUCTURAL LOADS IN AN AEROELASTIC AIRCRAFT |
ICAS 2008-7.7.2 |
| Carlomagno, G. M. |
EXPERIMENTAL ANALYSIS OF THE FLOW FIELD IN A ROTATING 'U' CHANNEL |
ICAS 2008-4.6.3 |
| Carpenter, A. L. |
FLIGHT EXPERIMENTS ON SWEPT WING TRANSITION USING DISTRIBUTED ROUGHNESS |
ICAS 2008-2.7.5 |
| Cassano, C. L. |
APPLICATION OF THE INTEGRATED PRODUCT TEAM (IPT) CONCEPT TO THE RE-ENGINE OF A VERY LIGHT JET (VLJ) |
ICAS 2008-6.7.5 |
| Castelletti, L. M. L. |
SURVEY OF FEASIBLE NUMERICAL APPROACHES TO ANALYSE THE BEHAVIOUR OF A COMPOSITE SKIN PANEL DURING A WATER IMPACT |
ICAS 2008-7.9.2 |
| Castelletti, L.-M. L. |
BIRDSTRIKE ONTO STRUCTURES IN ROTATIONAL MOTION |
ICAS 2008-9.4.4 |
| Castelli, L. |
CONTRACT-BASED AIR TRANSPORTATION SYSTEM TO FULFILL THE ARRIVING-ON-TIME OBJECTIVE |
ICAS 2008-8.2.1 |
| Catalano, F. M. |
AERO-STRUCTURAL MDO OF A SPAR-TANK-TYPE WING FOR AIRCRAFT CONCEPTUAL DESIGN |
ICAS2008-1.1 ST: |
| Catalano, F. M. |
PASSIVE, ACTIVE AND ADAPTIVE SYSTEMS FOR WING VORTEX DRAG REDUCTION |
ICAS2008-2.7 ST: |
| Cavagna, L. |
CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
| Cavagna, L. |
DEVELOPMENT AND VALIDATION OF A NEXT-GENERATION CONCEPTUAL AERO-STRUCTURAL SIZING SUITE |
ICAS 2008-1.6.2 |
| Cavagna, L. |
DEVELOPMENT AND VALIDATION OF AN INVESTIGATION TOOL FOR NONLINEAR AEROELASTIC ANALYSIS |
ICAS 2008-9.6.3 |
| Cecrdle, J. |
EXPLOITATION OF OPTIMIZATION SOLUTION FOR DETERMINATION OF WHIRL FLUTTER STABILITY BOUNDARIES |
ICAS2008-P3.2 |
| Cenko, A. |
STORE SEPARATION TRAJECTORY SIMULATION FOR THE HIGH SPEED ANTI-RADIATION DEMONSTRATOR (HSAD) FROM THE F-4 AIRCRAFT |
ICAS 2008-2.9.3 |
| Cenko, A. |
TARGETING PODS EFFECTS ON STORE SEPARATION CHARACTERISTICS: A JOINT NRC-IAR/USNAVY CFD EFFORT |
ICAS 2008-2.9.2 |
| Cerón-Muñoz, H. D. |
PASSIVE, ACTIVE AND ADAPTIVE SYSTEMS FOR WING VORTEX DRAG REDUCTION |
ICAS2008-2.7 ST: |
| Chai, J. Z. |
A FAST GRID DEFORMATION ALGORITHM AND IT’S APPLICATION |
ICAS2008-P2.4 |
| Chamberlain, J. P. |
PILOT IN-TRAIL PROCEDURE VALIDATION SIMULATION STUDY |
ICAS 2008-10.5.2 (AIAA 2008-8896) |
| Chambliss, A. |
AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
| Chang, J. -W. |
A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
| Charrier, J. -J. |
PARAMETRIC MODELING OF AN ELECTRICAL TEST RIG FOR POWER OPTIMIZED AIRCRAFT ARCHITECTURES |
ICAS2008-6.6 ST (AIAA 2008-8973) |
| Charrier, J.-J. |
A VISION OF MORE ELECTRICAL AIRCRAFT AND CURRENT DEVELOPMENTS |
ICAS 2008-6.5.1 INVITED |
| Chartrand, R. |
PILOT IN-TRAIL PROCEDURE VALIDATION SIMULATION STUDY |
ICAS 2008-10.5.2 (AIAA 2008-8896) |
| Chartrand, R. C. |
OPERATIONAL IMPROVEMENTS FROM IN-TRAIL PROCEDURE IN THE NORTH ATLANTIC ORGANIZED TRACK SYSTEM |
ICAS 2008-11.6.1 (AIAA 2008-8898) |
| Chate, A. |
METAMODELS FOR THE OPTIMIZATION OF DAMAGE-TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.3.3 |
| Chatterjee, T. |
LASER PROPELLED HYPERSONIC AIR-VEHICLE |
ICAS2008-4.3 ST: |
| Chen, B. |
AN APPROXIMATION METHOD FOR THE NUMERICAL SIMULATION ON UNSTEADY FLOWS AROUND SMALL-DISPLACEMENT MOVING OBJECTS |
ICAS2008-3.9 ST: |
| Chen, C. |
THE APPLICATION OF AIRBORNE VIDEO TECHNOLOGIES DURING AERIAL REFUELING TEST |
ICAS2008-P5.2 |
| Chen, N. Y. |
ESTIMATION OF AIR TRAFFIC DELAY USING THREE DIMENSIONAL WEATHER INFORMATION |
ICAS 2008-10.7.3 (AIAA 2008-8916) |
| Chen, Z. |
EFFECTS OF SUSPENSION WEIGHT ON FIGHTER FATIGUE DAMAGE |
ICAS 2008-7.4.5 |
| Cheng, H. |
TEST DATA MANAGEMENT FOR AIRCRAFT HYDRAULIC SYSTEM TESTING |
ICAS2008-P6.3 |
| Cheng, V. H. L. |
MODEL-BASED AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.1 (AIAA 2008-8907) |
| Cheng, V. H. L. |
QUEUEING NETWORK MODELS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.10.3 (AIAA 2008-8942) |
| Cheng, W. |
ADVANCED MANUFACTURING GRID SUPPORTING AVIATION INDUSTRY EXTENSIVE COLLABORATIVE DESIGN AND SIMULATION |
ICAS2008-6.10 ST: |
| Cheng, W. |
RESEARCH ON FAILURE CRITERION FOR COMPOSITE MATERIALS IN OPTIMIZATION |
ICAS 2008-7.1.2 |
| Cherevko, A. |
MODERN MATHEMATICAL METHODS IN AERONAUTICAL SCIENCES |
ICAS2008-2.3 ST: |
| Chiesa, S. |
ALTERNATIVE ENERGY BASED SYSTEMS FOR ADVANCED U.A.V.; THE “SAVE” PROJECT |
ICAS2008-6.6 ST: |
| Chishty, W. A. |
DEVELOPMENT OF AN INDUSTRIAL SCALE COMBUSTION TEST AND RESEARCH FACILITY FOR ALTERNATIVE FUELS AND FUEL FLEXIBILITY DEMONSTRATION |
ICAS 2008-4.3.1 |
| Cho, G. -H. |
A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
| Cho, J. |
UNSTEADY AERODYNAMIC ANALYSIS OF HELICOPTER ROTOR BY USING THE TIME-DOMAIN PANEL METHOD |
ICAS2008-2.10 ST: |
| Cho, L. |
UNSTEADY AERODYNAMIC ANALYSIS OF HELICOPTER ROTOR BY USING THE TIME-DOMAIN PANEL METHOD |
ICAS2008-2.10 ST: |
| Cho, S. H. |
BWB MILITARY CARGO TRANSPORT FUSELAGE DESIGN AND ANALYSIS |
ICAS 2008-7.9.3 |
| Chrishti, M. |
INVESTIGATION OF ADHESIVELY BONDED COMPOSITE STRUCTURE JOINTS |
ICAS 2008-7.2.1 |
| Chu, Y. -C. |
AUTOMATED CONFLICT RESOLUTION - A SIMULATION-BASED SENSITIVITY STUDY OF AIRSPACE AND DEMAND |
ICAS 2008-8.9.1 |
| Chung, S. |
NATSIM: A SYSTEMS DYNAMICS MODEL OF NORTH ATLANTIC AIR TRAFFIC |
ICAS 2008-9.11.3 (AIAA 2008-8912) |
| Chupakhin, A. |
MODERN MATHEMATICAL METHODS IN AERONAUTICAL SCIENCES |
ICAS2008-2.3 ST: |
| Cisowski, J. |
MINI UAV DESIGN AND OPTIMIZATION FOR LONG ENDURANCE MISSION |
ICAS 2008-1.5.2 |
| Clare, J. C. |
A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
| Clarke, A. |
DESIGN AND DEVELOPMENT OF THE ECLIPSE AND DEMON DEMONSTRATOR UAVS |
ICAS 2008-1.4.2 |
| Claus, R. W. |
COUPLED HIGH-FIDELITY ENGINE SYSTEM SIMULATION |
ICAS 2008-8.10.3 INVITED |
| Clay, S. |
FLIGHT VEHICLE COMPOSITE STRUCTURES |
ICAS 2008-7.9.1 (AIAA 2008-8976 ) |
| Coatanéa, M. |
PRELIMINARY DESIGN OF A JOINED WING HALE UAV |
ICAS 2008-1.4.3 |
| Coimbra, R. F. |
PASSIVE, ACTIVE AND ADAPTIVE SYSTEMS FOR WING VORTEX DRAG REDUCTION |
ICAS2008-2.7 ST: |
| Coiro, D. P. |
SINGLE VERSUS MULTIPLE WINGLETS: NUMERICAL AND EXPERIMENTAL INVESTIGATION |
ICAS 2008-2.7.3 |
| Collisson, C. |
RE-INVENTING THE LEGEND: THE DEVELOPMENT OF THE 747-8 |
ICAS 2008-1.7.3 |
| Cologan, C. |
AERODYNAMIC INVESTIGATIONS ON A GENERIC FAN-IN-WING CONFIGURATION |
ICAS 2008-3.5.1 |
| Comell, B. |
TAILORED ARRIVALS OPERATIONS AT SFO AND EXPECTED ENVIRONMENTAL BENEFITS |
ICAS 2008-11.3.4 (AIAA 2008-8868) |
| Consiglio, M. |
IMPACT OF PREDICTION UNCERTAINTY ON THE SAFETY PERFORMANCE OF AIRBORNE SEPARATION |
ICAS 2008-11.4.2 (AIAA 2008-8882) |
| Conway, S. R. |
TOWARDS 4D TRAJECTORY MANAGEMENT: CONTAINMENT AND THE USE OF RNP IN CONSTRAINED TERMINAL AIRSPACE |
ICAS2008-8.11 ST: |
| Cook, L. S. |
IMPROVED PREDICTION OF GATE DEPARTURE TIMES USING PRE-DEPARTURE EVENTS |
ICAS 2008-11.8.1 (AIAA 2008-8919) |
| Cordisco, P. |
METAMODELS FOR THE OPTIMIZATION OF DAMAGE-TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.3.3 |
| Corke, T. C. |
FOREBODY VORTEX CONTROL ON HIGH PERFORMANCE AIRCRAFT USING PWM-CONTROLLED PLASMA ACTUATORS |
ICAS 2008-3.3.4 |
| Corpino, S. |
ALTERNATIVE ENERGY BASED SYSTEMS FOR ADVANCED U.A.V.; THE “SAVE” PROJECT |
ICAS2008-6.6 ST: |
| Crescenzio, F.De |
DESIGN AND EVALUATION OF A 4D INTERFACE FOR ATC |
ICAS 2008-9.10.3 |
| Crook, I. |
MULTI-OBJECTIVE OPTIMIZATION OF USER PREFERRED 4D TRAJECTORIES IN THE NAS |
ICAS 2008-11.6.2 (AIAA 2008-8899) |
| Crossley, W. |
COMBINATORIAL OPTIMIZATION TO INCLUDE GREENER TECHNOLOGIES IN A SHORT-TO-MEDIUM RANGE COMMERCIAL AIRCRAFT |
ICAS 2008-4.10.2 (AIAA 2008-8963) |
| Crossley, W. A. |
BASE OF OPERATIONS CONCEPT FOR ON-DEMAND OPERATIONS |
ICAS 2008-8.6.4 (AIAA 2008-8977 ) |
| Crossley, W. A. |
CONCURRENT AIRCRAFT DESIGN AND RESOURCE ALLOCATION UNDER UNCERTAINTY FOR ON-DEMAND AIR TRANSPORTATION |
ICAS 2008-10.6.1 (AIAA 2008-8903) |
| Cui, D. |
ADVANCED MANUFACTURING GRID SUPPORTING AVIATION INDUSTRY EXTENSIVE COLLABORATIVE DESIGN AND SIMULATION |
ICAS2008-6.10 ST: |
| Cui, D. |
RESEARCH ON FAILURE CRITERION FOR COMPOSITE MATERIALS IN OPTIMIZATION |
ICAS 2008-7.1.2 |
| Curran, R. |
AEROSPACE PRODUCT COST MANAGEMENT AT THE EARLY CONCEPT OPERATIONS PHASE |
ICAS 2008-10.6.2 (AIAA 2008-8904) |
| Curran, R. |
AUTOMATED ASSEMBLY TIME ANALYSIS USING A DIGITAL KNOWLEDGE BASED APPROACH |
ICAS 2008-10.3.1 (AIAA 2008-8861) |
| Curran, R. |
LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
| Curran, R. |
USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
| Da Ronch, A. |
DEVELOPMENT AND VALIDATION OF A NEXT-GENERATION CONCEPTUAL AERO-STRUCTURAL SIZING SUITE |
ICAS 2008-1.6.2 |
| da Silva, R. G. |
AN AERODYNAMIC OPTIMIZATION FRAMEWORK BASED ON GENETIC ALGORITHMS |
ICAS 2008-2.3.4 |
| Dao, A. Q. |
ASSESSMENT OF FLIGHT CREW ACCEPTANCE OF AUTOMATED RESOLUTION SUGGESTIONS AND MANUAL RESOLUTION TOOLS |
ICAS 2008-8.7.2 |
| Dartois, S. |
A MULTI-SCALE “MORPHOLOGICAL APPROACH” FOR MODELING THE NON LINEAR BEHAVIOR OF PROPELLANT-LIKE MATERIALS |
ICAS 2008-7.1.3 |
| De Crescenzio, F. |
3D OBSTACLE AVOIDANCE STRATEGIES FOR UAS (UNINHABITED AERIAL SYSTEMS) MISSION PLANNING AND RE-PLANNING |
ICAS 2008-5.6.1 (AIAA 2008-8962) |
| De Crescenzio, F. |
DESIGN AND DEVELOPMENT OF AN ATC DISTRIBUTED TRAINING SYSTEM |
ICAS2008-P8.2 (AIAA 2008-8873) |
| de Gelder, N. |
ENABLING TECHNOLOGY EVALUATION FOR EFFICIENT CONTINUOUS DESCENT APPROACHES |
ICAS 2008-8.9.2 |
| de Jong, H. H. |
A PROGNOSTIC METHOD TO IDENTIFY HAZARDS FOR FUTURE AVIATION CONCEPTS |
ICAS 2008-9.3.1 |
| de Jong, J. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
| de Kat, R. |
VORTEX WAKE INVESTIGATION BEHIND A WING-FLAP MODEL WITH JET SIMULATION |
ICAS 2008-3.9.1 |
| de Muynck, R. J. |
ENABLING TECHNOLOGY EVALUATION FOR EFFICIENT CONTINUOUS DESCENT APPROACHES |
ICAS 2008-8.9.2 |
| de Oliveira Neto, J. A. |
APPLICATION OF A NAVIER-STOKES CODE TO THE SIMULATIONS OF HIGH-LIFT DEVICES USING UNSTRUCTURED GRIDS |
ICAS 2008-2.2.4 |
| De Tenorio, C. |
FUNCTION BASED ARCHITECTURE DESIGN SPACE DEFINITION AND EXPLORATION |
ICAS 2008-1.9.3 (AIAA 2008-8928) |
| de Tenorio, C. |
METHODOLOGY FOR AIRCRAFT SYSTEM ARCHITECTURE SIZING |
ICAS 2008-6.2.2 |
| De Visscher, I. |
AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION FOR TAKE-OFF AND DEPARTURE |
ICAS 2008-11.8.3 (AIAA 2008-8921) |
| de Ward, A. |
DESIGN OF A LEAN MRO BUSINESS PROCESS FOR EPCOR |
ICAS 2008-10.3.4 (AIAA 2008-8864) |
| de Witte, T. D. |
A PRACTICAL APPROACH TO MULTI-OBJECTIVE CAPACITY ANALYSIS OF AN ENVIRONMENT-AWARE AIRPORT |
ICAS 2008-8.5.1 |
| DeArmon, J. |
AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
| Decours, J. |
AERODYNAMIC AND AERO-ACOUSTIC DESIGN OF MODERN TILT-ROTORS: THE ONERA EXPERIENCE |
ICAS 2008-1.7.4 |
| DeGarmo, M. |
NEXTGEN AND SESAR: OPPORTUNITIES FOR UAS INTEGRATION |
ICAS 2008-10.8.2 (AIAA 2008-8925) |
| Degenhardt, R. |
COLLAPSE BEHAVIOR OF THIN-WALLED CFRP STRUCTURES DUE TO MATERIAL AND GEOMETRIC NONLINEARITIES–EXPERIMENTS AND SIMULATION |
ICAS 2008-7.11.3 |
| Degenhardt, R. |
THE DESIGN OF POSTBUCKLING COMPOSITE AEROSPACE STRUCTURES ACCOUNTING FOR DAMAGE INITIATION AND GROWTH |
ICAS 2008-7.3.2 |
| Delannoy, A. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
| DeLaurentis, D. A. |
A NEW SYSTEMS ANALYSIS: PERSPECTIVES ON SYSTEM-OF-SYSTEMS AND REGIONAL TRANSPORTATION PROOF-OF-CONCEPT STUDY |
ICAS 2008-1.3.2 |
| DeLaurentis, D. A. |
UTILIZATION OF NETWORK THEORY FOR THE ENHANCEMENT OF ATO AIR ROUTE FORECAST |
ICAS 2008-11.10.5 (AIAA 2008-8944) |
| Deligiannidis, N. |
MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
| Deloach, R. |
ESTIMATION OF SUPERSONIC STAGE SEPARATION AERODYNAMICS OF WINGED-BODY LAUNCH VEHICLES USING RESPONSE SURFACE METHODS |
ICAS 2008-3.1.1 |
| Denegri Jr., C. M. |
REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
| Deng, Y. C. |
OPTIMIZATION DESIGN ON PLATE-RIB STRUCTURE FOR CERTAIN KINDS OF AIRCRAFT |
ICAS 2008-9.5.3 |
| Deremaux, Y. |
DESIGN OF A SMALL SUPERSONIC TRANSPORT AIRCRAFT WITH HIGH ENVIRONMENTAL CONSTRAINTS |
ICAS 2008-1.10.1 INVITED |
| Deremeaux, Y. |
UNCERTAINTIES AT THE CONCEPTUAL STAGE: MULTILEVEL MULTIDISCIPLINARY DESIGN AND OPTIMIZATION APPROACH |
ICAS 2008-1.1.2 |
| Deslandes, R. |
IHAAA STORE SEPARATION FROM CAVITY (SSC) PROJECT |
ICAS 2008-2.6.2 |
| d'Espiney, P. |
WHITE LIGHT SKIN-FRICTION AND GAS DENSITY MEASUREMENTS AROUND A SUPERSONIC FOREBODY |
ICAS 2008-3.8.2 |
| Desse, J. M. |
WHITE LIGHT SKIN-FRICTION AND GAS DENSITY MEASUREMENTS AROUND A SUPERSONIC FOREBODY |
ICAS 2008-3.8.2 |
| Devenny, C. |
USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
| Di Cicca, G. M. |
LARGE-SCALE MANIPULATION OF A TURBULENT BOUNDARY LAYER BY MEANS OF A 2D SYNTHETIC JET |
ICAS2008-P2.8 |
| Di Landro, L. |
DESIGN AND MANUFACTURING OF COMPOSITE CHIRAL STRUCTURES WITH MORPHING CAPABILITIES |
ICAS 2008-7.8.1 |
| Díaz, J. |
THERMAL DESIGN UNDER UNCERTAINTIES OF AIRCRAFT STRUCTURES |
ICAS 2008-7.2.3 |
| Dignum, V. |
AN ONTOLOGY FOR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-9.11.1 (AIAA 2008-8946) |
| Dillenius, M. |
IHAAA STORE SEPARATION FROM CAVITY (SSC) PROJECT |
ICAS 2008-2.6.2 |
| Dinh, Q. V. |
UNCERTAINTIES AT THE CONCEPTUAL STAGE: MULTILEVEL MULTIDISCIPLINARY DESIGN AND OPTIMIZATION APPROACH |
ICAS 2008-1.1.2 |
| Dircken, F. |
CONTROLLABILITY OF BLENDED WING BODY AIRCRAFT |
ICAS 2008-5.4.3 |
| Djojodihardjo, H. |
UNIFIED BE-FE AERODYNAMIC-ACOUSTIC-STRUCTURE COUPLING SCHEME FOR ACOUSTIC EFFECTS ON AEROELASTIC STRUCTURES |
ICAS 2008-7.7.3 |
| Doble, N. A. |
CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
| Dodbelle, S. |
STORE SEPARATION TRAJECTORY SIMULATION FOR THE HIGH SPEED ANTI-RADIATION DEMONSTRATOR (HSAD) FROM THE F-4 AIRCRAFT |
ICAS 2008-2.9.3 |
| Doherty, J. |
LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
| Doll, C. |
MODELLING OF THE 3-DOF NONLINEAR AIRCRAFT BEHAVIOUR VIA SMALL STANDARD FORMS |
ICAS2008-P5.5 |
| Domino, D. A. |
SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
| Donnerhack, S. |
A NEW APPROACH FOR CO2 REDUCTION APPLYING STATE-OF-THE-ART ENGINE AND AIRFRAME TECHNOLOGY |
ICAS2008-4.2 ST (AIAA 2008-8974) |
| Dorgan, A. |
A HYBRID, DYNAMIC LARGE EDDY SIMULATION METHOD |
ICAS 2008-2.1.1 |
| Dowell, E. H. |
REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
| Dr?g??anu, C. |
AUTOMATIC FLIGHT CONTROL USING SAMPLED-DATA MIXED H_2/H_INFINITY OPTIMISATION |
ICAS 2008-5.2.1 |
| Dragon, A. |
A MULTI-SCALE “MORPHOLOGICAL APPROACH” FOR MODELING THE NON LINEAR BEHAVIOR OF PROPELLANT-LIKE MATERIALS |
ICAS 2008-7.1.3 |
| Dray, L. |
MODELLING AIRLINE ROUTING AND SCHEDULING UNDER AIRPORT CAPACITY CONSTRAINTS |
ICAS 2008-11.1.2 (AIAA 2008-8855) |
| Dray, L. M. |
NETWORK AND ENVIRONMENTAL IMPACTS OF PASSENGER AND AIRLINE RESPONSE TO COST AND DELAY |
ICAS 2008-10.4.4 (AIAA 2008-8890) |
| Dron, S. |
TOWARD ACARE 2020: INNOVATIVE ENGINE ARCHITECTURES TO ACHIEVE THE ENVIRONMENTAL GOALS? |
ICAS 2008-4.2.2 |
| Duan, X. |
TERRAIN FOLLOWING FLIGHT REAL-TIME HIL SIMULATION PLATFORM RESEARCH |
ICAS2008-P5.6 |
| Duffy, M. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
| Duong, V. |
ANALYSIS OF GAPS BETWEEN THE PREDICTIVE AND THE ADAPTIVE COMPONENT IN ATM |
ICAS 2008-11.10.2 (AIAA 2008-8941) |
| Duong, V. |
HARMONIZING AUTOMATION, PILOT AND AIR TRAFFIC CONTROLLER IN THE FUTURE AIR TRAFFIC MANAGEMENT |
ICAS 2008-8.2.4 |
| D'Urso, S. D. |
FLIGHT DYNAMICS OF THE FLYING WING |
ICAS 2008-5.8.3 |
| Dwight, R. P. |
NUMERICAL AERODYNAMIC OPTIMISATIONS OF 3D HIGH-LIFT CONFIGURATIONS |
ICAS 2008-2.2.3 |
| Early, J. M. |
EXCRESCENCES EFFECTS IN AERODYNAMICS |
ICAS2008-3.8 ST: |
| Edinger, C. |
INNOVATIVE FUTURE AIR TRANSPORT SYSTEM: SIMULATION OF A FULLY AUTOMATED ATS |
ICAS 2008-8.4.5 |
| Edinger, C. |
PERFORMANCE-BASED TMA HANDLING FOR MIXED TRAFFIC USING A GROUND BASED 4D-GUIDANCE FOR UNEQUIPPED AIRCRAFT |
ICAS 2008-10.8.3 |
| Egami, Y. |
DEVELOPMENT & APPLICATION OF MODERN MEASUREMENT TECHNIQUES FOR PRESSURIZED CRYOGENIC WIND TUNNELS |
ICAS 2008-3.2.1 |
| Egbert, N. |
DESIGN FOR PROCESS EXCELLENCE - ENSURING TIMELY AND COST EFFECTIVE SOLUTIONS |
ICAS 2008-6.7.4 |
| Eglitis, E. |
METAMODELS FOR THE OPTIMIZATION OF DAMAGE-TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.3.3 |
| Eijgelshoven, T. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
| Elangovan, R. |
MODELING OF ACOUSTICALLY TREATED NACELLE LIP TRANSPIRATION FLOW ANTI-ICING SYSTEM |
ICAS 2008-6.4.3 |
| Elfstrom, G. M. |
DESIGN AND OPERATION OF THE ADD ENVIRONMENTAL TEST FACILITY |
ICAS2008-P6.6 |
| Elliff, T. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
| Elmer, K. R. |
TAILORED ARRIVALS OPERATIONS AT SFO AND EXPECTED ENVIRONMENTAL BENEFITS |
ICAS 2008-11.3.4 (AIAA 2008-8868) |
| Empringham, L. |
A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
| Engelland, S. A. |
MICROSCOPIC ANALYSIS OF AIRPORT SURFACE SEQUENCING |
ICAS2008-11.11 ST (AIAA 2008-8961) |
| Engert, M. |
ACTIVE CANCELLATION OF TOLLMIEN-SCHLICHTING INSTABILITIES UP TO M = 0.40 |
ICAS 2008-3.10.2 |
| Entzinger, J. O. |
MODELING OF THE VISUAL APPROACH TO LANDING USING NEURAL NETWORKS AND FUZZY SUPERVISORY CONTROL |
ICAS 2008-5.1.3 |
| Epstein, B. |
EFFICIENT APPROACH FOR MULTIPOINT AERODYNAMIC WING DESIGN OF BUSINESS JET AIRCRAFT |
ICAS 2008-2.11.1 |
| Epstein, B. |
HYBRIDIZATION OF HETEROGENEOUS 3D CFD DISCRETIZATIONS VIA DIRECT FLUX OPTIMIZATION |
ICAS2008-2.3 ST: |
| Erdem, E. |
THE INVESTIGATION OF DEPENDENCE OF LOW FREQUENCY MOTION ON UPSTREAM FLOW CONDITIONS IN HYPERSONIC FLOWS |
ICAS2008-3.7 ST: |
| Erickson, G. |
ESTIMATION OF SUPERSONIC STAGE SEPARATION AERODYNAMICS OF WINGED-BODY LAUNCH VEHICLES USING RESPONSE SURFACE METHODS |
ICAS 2008-3.1.1 |
| Eriksen, P. |
OPERATIONAL CONCEPT FOR AN AIRPORT OPERATIONS CENTER TO ENABLE TOTAL AIRPORT MANAGEMENT |
ICAS 2008-8.3.2 |
| Erzberger, H. |
ALGORITHM AND OPERATIONAL CONCEPT FOR RESOLVING SHORT-RANGE CONFLICTS |
ICAS 2008-8.7.5 |
| Erzberger, H. |
AUTOMATED CONFLICT RESOLUTION - A SIMULATION-BASED SENSITIVITY STUDY OF AIRSPACE AND DEMAND |
ICAS 2008-8.9.1 |
| Estkowski, R. |
REAL-TIME SIMULATION OF A DISTRIBUTED CONFLICT RESOLUTION ALGORITHM |
ICAS 2008-8.7.3 |
| Evans, A. |
NETWORK AND ENVIRONMENTAL IMPACTS OF PASSENGER AND AIRLINE RESPONSE TO COST AND DELAY |
ICAS 2008-10.4.4 (AIAA 2008-8890) |
| Evans, A. D. |
MODELLING AIRLINE ROUTING AND SCHEDULING UNDER AIRPORT CAPACITY CONSTRAINTS |
ICAS 2008-11.1.2 (AIAA 2008-8855) |
| Everdij, M. H. C. |
A PROGNOSTIC METHOD TO IDENTIFY HAZARDS FOR FUTURE AVIATION CONCEPTS |
ICAS 2008-9.3.1 |
| Eyers, C. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
| Fabiani, P. |
PERSPECTIVES ON (MULTI-) UAV OPERATIONS: AUTONOMY & SECURITY ISSUES |
ICAS 2008-6.8.3 INVITED |
| Falk, R. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
| Faller, W. E. |
SIMULATION OF A NON-AXISYMMETRIC UNDERSEA VEHICLE USING A RECURSIVE NEURAL NETWORK |
ICAS 2008-5.8.2 |
| Fanget, A. |
A MULTI-SCALE “MORPHOLOGICAL APPROACH” FOR MODELING THE NON LINEAR BEHAVIOR OF PROPELLANT-LIKE MATERIALS |
ICAS 2008-7.1.3 |
| Farahmand, B. |
COHESIVE DISINTEGRATION IN IMPACTED RE-ENTRY SPACE TRANSPORTATION HYBRID STRUCTURES |
ICAS 2008-7.5.1 |
| Farahmand, R. |
PREDICTION OF DELAMINATION IN ADVANCED AEROSPACE COMPOSITE STRUCTURES USING MICRO/MACRO MECHANICS CONSTITUTIVE METHODS |
ICAS 2008-7.5.3 |
| Farley, T. |
AUTOMATED CONFLICT RESOLUTION - A SIMULATION-BASED SENSITIVITY STUDY OF AIRSPACE AND DEMAND |
ICAS 2008-8.9.1 |
| Fasano, G. |
DEVELOPMENT AND TEST OF AN INTEGRATED SENSOR SYSTEM FOR AUTONOMOUS COLLISION AVOIDANCE |
ICAS2008-P6.12 |
| Fasel, H. F. |
INVESTIGATION OF SEPARATION CONTROL FOR LOW-PRESSURE TURBINES USING CFD |
ICAS 2008-4.4.2 |
| Fazli, N. |
EFFECTS OF HIERARCHY ORDER ON NATURAL FREQUENCY AND VIBRATION TRANSMISSION OF SELF-SIMILAR TRUSSES |
ICAS2008-P3.9 |
| Feih, S. |
LOADED CARBON COMPOSITE SCARF JOINTS SUBJECT TO QUASI STEADY LATERAL LOADS |
ICAS 2008-7.2.2 |
| Feldman, G. R. |
VISAGE - A NEW VISION FOR GEOSPATIAL DATA VISUALIZATION AND ANALYSIS |
ICAS2008-P8.1 (AIAA 2008-8872) |
| Féru, F. |
SYSTEM INFRASTRUCTURE FOR INTEGRATED AND COLLABORATIVE PRODUCT DEVELOPMENT IN THE AERONAUTIC INDUSTRY |
ICAS 2008-6.10.2 |
| Fey, U. |
DEVELOPMENT & APPLICATION OF MODERN MEASUREMENT TECHNIQUES FOR PRESSURIZED CRYOGENIC WIND TUNNELS |
ICAS 2008-3.2.1 |
| Fielding, J. P. |
DESIGN AND DEVELOPMENT OF THE ECLIPSE AND DEMON DEMONSTRATOR UAVS |
ICAS 2008-1.4.2 |
| Fielding, J. P. |
NOVEL DESIGN CONCEPTS FOR AIRCRAFT WITH REDUCED NOISE AND GLOBAL WARMING CHARACTERISTICS |
ICAS 2008-4.10.4 |
| Fielding, J. P. |
RECENT DEVELOPMENTS OF MSG-3 (MAINTANANCE STEERING GROUP) GUIDANCE FOR THE CONTINUED AIRWORTHINESS OF LIGHTNING/HIRF PROTECTION AND BENFITS TO NEW AIRPLANE DESIGN |
ICAS 2008-9.4.5 (AIAA 2008-8964 ) |
| Filatyev, A. S. |
AEROSPACE TRAJECTORY OPTIMIZATION: NOVEL VIEW ON A ROLE OF ATMOSPHERIC FLIGHT |
ICAS 2008-5.3.1 |
| Fleming, G. |
PAYLOAD FUEL ENERGY EFFICIENCY AS A METRIC FOR AVIATION ENVIRONMENTAL PERFORMANCE |
ICAS 2008-4.7.4 |
| Fleming, G. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
| Fofonov, D. |
NUMERICAL SIMULATION OF VISCOUS FLOWS AROUND LIFTING BODIES OF COMPLICATED CONFIGURATION |
ICAS 2008-2.6.3 |
| Follet, J. |
TAILORED ARRIVALS OPERATIONS AT SFO AND EXPECTED ENVIRONMENTAL BENEFITS |
ICAS 2008-11.3.4 (AIAA 2008-8868) |
| Fong, C. -C. V. |
SECURE AIRSPACE: A CRITICAL COMPONENT OF NEXTGEN'S LAYERED, ADAPTIVE SECURITY |
ICAS 2008-11.5.2 (AIAA 2008-8893) |
| Fong, R. K. |
DEVELOPMENT AND APPLICATION OF AN INTEGRATED APPROACH TOWARD NASA AIRSPACE SYSTEMS RESEARCH |
ICAS 2008-10.8.1 (AIAA 2008-8924) |
| Fonseca, A. |
ON THE DEVELOPMENT OF METHODS AND TECHNIQUES FOR AIRCRAFT STRUCTURAL HEALTH MONITORING |
ICAS2008-7.4 ST: |
| Forster, C. |
AN INTEGRATED USER-ORIENTED WEATHER FORECAST SYSTEM FOR AIR TRAFFIC USING REAL-TIME OBSERVATIONS AND MODEL DATA |
ICAS 2008-8.6.3 |
| Forster, C. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
| Forster, E. |
FLIGHT VEHICLE COMPOSITE STRUCTURES |
ICAS 2008-7.9.1 (AIAA 2008-8976 ) |
| Fortin, F. |
TARGETING PODS EFFECTS ON STORE SEPARATION CHARACTERISTICS: A JOINT NRC-IAR/USNAVY CFD EFFORT |
ICAS 2008-2.9.2 |
| Francesconi, E. |
SURVEY OF FEASIBLE NUMERICAL APPROACHES TO ANALYSE THE BEHAVIOUR OF A COMPOSITE SKIN PANEL DURING A WATER IMPACT |
ICAS 2008-7.9.2 |
| Francis, M. S. |
DESIGN OF NEXT GENERATION UNMANNED AIR SYSTEMS - ISSUES AND OPPORTUNITIES |
ICAS 2008-1.4.1 INVITED |
| Friehmelt, H. |
KEY EXAMPLES AND POTENTIAL OF AVIATION YOUTH PROGRAMS IN GERMANY |
ICAS 2008-6.9.3 |
| Frossard, P. L. |
SYSTEM INFRASTRUCTURE FOR INTEGRATED AND COLLABORATIVE PRODUCT DEVELOPMENT IN THE AERONAUTIC INDUSTRY |
ICAS 2008-6.10.2 |
| Frota, J. |
NACRE EUROPEAN PROJECT PROGRESS SUMMARY |
ICAS 2008-1.7.2 |
| Fry, D. N. |
A NEW SYSTEMS ANALYSIS: PERSPECTIVES ON SYSTEM-OF-SYSTEMS AND REGIONAL TRANSPORTATION PROOF-OF-CONCEPT STUDY |
ICAS 2008-1.3.2 |
| Frydrychewicz, A. |
MINI UAV DESIGN AND OPTIMIZATION FOR LONG ENDURANCE MISSION |
ICAS 2008-1.5.2 |
| Fukuda, Y. |
DESIGN OF OPERATION DATABASE FOR ATM PERFORMANCE ASSESSMENT |
ICAS 2008-8.9.4 |
| Fumagalli, A. |
BIOMECHANICAL PILOT PROPERTIES IDENTIFICATION BY INVERSE KINEMATICS/INVERSE DYNAMICS MULTIBODY ANALYSIS |
ICAS 2008-9.10.4 |
| Fürstenau, N. |
AUGMENTED VISION VIDEOPANORAMA SYSTEM FOR REMOTE AIRPORT TOWER OPERATION |
ICAS 2008-8.3.1 |
| Gaertner, N. |
ON-DEMAND SPECIAL USE AIRSPACE |
ICAS 2008-10.10.4 (AIAA 2008-8938) |
| Gai, S. L. |
DRAG AND FLOW REGIMES ASSOCIATED WITH RECTANGULAR CAVITIES AT YAW AT LOW SPEEDS |
ICAS2008-P2.13 |
| Galaktionov, A. |
NUMERICAL SIMULATION OF VISCOUS FLOWS AROUND LIFTING BODIES OF COMPLICATED CONFIGURATION |
ICAS 2008-2.6.3 |
| Galbraith, R. A . McD. |
PERFORMANCE DEGRADATION OF A SIMULATED ICE CONTAMINATED AIRFOIL BY SUPER-COOLED DROPLETS |
ICAS 2008-3.7.2 |
| Gallo, M. |
EXPERIMENTAL ANALYSIS OF THE FLOW FIELD IN A ROTATING 'U' CHANNEL |
ICAS 2008-4.6.3 |
| Gao, C. |
TRANSONIC FLUTTER ANALYSIS OF AN AIRFOIL WITH APPROXIMATE BOUNDARY METHOD |
ICAS 2008-7.10.5 |
| Gao, Z. |
THE APPLICATION OF ASEXUAL DNA ALGORITHM TO AIRFOIL DESIGN |
ICAS 2008-2.3.3 |
| Gao, Z. H |
RESEARCH ON CONTROL ALLOCATION FOR AIRCRAFTS WITH MULTIPLE CONTROL EFFECTORS |
ICAS 2008-5.2.4 |
| Gao, Z. H. |
RESEARCH ON FUZZY LOGIC PIO DETECTOR |
ICAS 2008-5.4.5 |
| Garcia, A. N. |
SIMPLIFYING MSD MODELING BY USING CONTINUING DAMAGE ASSUMPTION AND PARAMETRIC STUDY: THE ROLE OF RIVET SQUEEZE FORCE |
ICAS 2008-9.8.1 |
| Garcia, E |
FUNCTION BASED ARCHITECTURE DESIGN SPACE DEFINITION AND EXPLORATION |
ICAS 2008-1.9.3 (AIAA 2008-8928) |
| Garcia, E. |
A METHODOLOGICAL APPROACH FOR AIRPORT TECHNOLOGY EVALUATION AND SELECTION |
ICAS 2008-8.3.4 (AIAA 2008-8965) |
| Garcia, E. |
METHODOLOGY FOR AIRCRAFT SYSTEM ARCHITECTURE SIZING |
ICAS 2008-6.2.2 |
| Garcia, E. |
PARAMETRIC MODELING OF AN ELECTRICAL TEST RIG FOR POWER OPTIMIZED AIRCRAFT ARCHITECTURES |
ICAS2008-6.6 ST (AIAA 2008-8973) |
| Garcia-Chico, J. L. |
TASK ANALYSIS FOR FEASIBILITY ASSESSMENT OF A COLLABORATIVE TRAFFIC FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.7.3 (AIAA 2008-8909) |
| Garrett, J. S. |
AVIATION TELEMEDICINE: PAST, PRESENT AND FUTURE |
ICAS 2008-9.2.2 |
| Gati, B. |
PARAMETER IDENTIFICATION OF FLYING WING WITH SIGNIFICANT DEFORMATION |
ICAS 2008-5.8.1 |
| Gatto, C. |
TRAJECTORY TRACKING FOR A NON - CONVENTIONAL UAV |
ICAS2008-P5.3 |
| Gauci, J. |
A RAPID SCENARIO GENERATION TOOL FOR REPEATABLE SIMULATED TRAFFIC CONFLICTS IN FLIGHT SIMULATION |
ICAS 2008-5.1.1 INVITED |
| Gauci, J. |
DESIGN OF EXPERIMENT FOR THE PILOT EVALUATION OF AN AIRBORNE RUNWAY INCURSION ALERTING SYSTEM |
ICAS 2008-9.10.2 |
| Gavel, H. |
A QUANTIFIED RELATIONSHIP MATRIX AIDED BY PROBABILISTIC DESIGN AND OPTIMIZATION |
ICAS 2008-6.2.1 |
| Gavrilets, V. |
DAMAGE TOLERANT FLIGHT CONTROL SYSTEMS FOR UNMANNED AIRCRAFT |
ICAS 2008-6.8.1 INVITED |
| Gawale, A. C. |
DESIGN, FABRICATION AND OPERATION OF REMOTELY CONTROLLED AIRSHIPS IN INDIA |
ICAS 2008-10.1.3 (AIAA 2008-8853) |
| Gehri, A. |
UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
| Genc, M. |
AN EXPERIMENTAL AND COMPUTATIONAL STUDY OF LOW RE NUMBER TRANSITIONAL FLOWS OVER AN AEROFOIL WITH LEADING EDGE SLAT |
ICAS2008-P2.1 (AIAA 2008-8877) |
| Gerz, T. |
PERFORMANCE OF THE WAKE VORTEX PREDICTION AND MONITORING SYSTEM WSVBS AT FRANKFURT AIRPORT |
ICAS 2008-8.11.2 |
| Ghavami, G. |
AN ANALYTICAL MODEL FOR PREDICTION OF THE STEADY STATE CREEP DEFORMATIONS AND STRESSES OF SHORT FIBER COMPOSITES |
ICAS 2008-9.8.3 |
| Ghedaifi, W. |
A NOVEL APPROACH TO AIR TRANSPORT SYSTEM ENVIRONMENTAL IMPACT EVALUATION THROUGH PHYSICAL MODELLING AND SIMULATION |
ICAS2008-8.3 ST: |
| Ghobbar, A. |
INTERMITTENT DEMAND FORECAST BY COMBINING THE FORECASTS FROM SEVERAL METHODS INTO A COMPOSITE ONE WITHIN MRO SECTOR |
ICAS 2008-10.3.3 (AIAA 2008-8863) |
| Ghoreyshi, M. |
CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
| Gier, J. |
PREPARING LP TURBINE TECHNOLOGY FOR MODERN AIRCRAFT ENGINES |
ICAS 2008-4.6.1 |
| Gilmour, M. |
AEROSPACE PRODUCT COST MANAGEMENT AT THE EARLY CONCEPT OPERATIONS PHASE |
ICAS 2008-10.6.2 (AIAA 2008-8904) |
| Giordano, R. |
MODULATION TRANSFER FUNCTION OF STEREO PARTICLE IMAGE VELOCIMETRY TECHNIQUE |
ICAS2008-P2.6 |
| Giris, S. |
DEVELOPING THE NEXT GENERATION OF GLOBAL GAS TURBINE ENGINEERS |
ICAS 2008-8.10.1 INVITED |
| Godiksen III, W. H. |
TARGETING POD EFFECTS ON WEAPONS RELEASE FROM THE F-18C HORNET |
ICAS 2008-2.9.4 |
| Goetzendorf-Grabowski, T. |
CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
| Golia, C. |
ANALYSIS OF THERMOCHEMICAL MODELING AND SURFACE CATALYTICITY IN SPACE VEHICLES REENTRY |
ICAS 2008-3.6.2 |
| Golia, C. |
VORTEX BLOB METHOD AS VISUALIZATION TOOL FOR MULTI-ELEMENT AIRFOIL FLOWS OPTIMIZATION |
ICAS 2008-3.9.2 |
| Golikov, A. A. |
AEROSPACE TRAJECTORY OPTIMIZATION: NOVEL VIEW ON A ROLE OF ATMOSPHERIC FLIGHT |
ICAS 2008-5.3.1 |
| Gollnick, V. |
A HOLISTIC APPROACH TO EVALUATE THE AIR TRANSPORTATION SYSTEM |
ICAS 2008-8.4.2 |
| Gologan, C. |
CONCEPTUAL DESIGN OF A STOL REGIONAL-JET WITH HYBRID PROPULSION SYSTEM |
ICAS 2008-1.2.1 |
| Gologan, C. |
IMPACT OF ESTOL CAPABILITY ON RUNWAY CAPACITY - AN ANALYTICAL APPROACH |
ICAS 2008-11.9.4 (AIAA 2008-8933) |
| Gomes da Costa, T. F. G. |
INFLUENCES INVESTIGATION OF NUMERICAL PARAMETERS AND MESHING ON THE AEROELASTIC RESPONSE |
ICAS2008- P3.4 |
| Gomes da Costa, T. F. G. |
NUMERICAL DEVELOPMENT OF A FLUTTER ACTIVE CONTROL SYSTEM BASED ON PRESSURE FEEDBACK. |
ICAS2008-P3.3 |
| Gonzalez-Perez, H. |
CAPACITY MODELLING FOR FUTURE AERONAUTICAL SAFETY COMMUNICATIONS OVER WIDE AREAS |
ICAS 2008-8.8.2 (AIAA 2008-8952) |
| Gooden, J. H. M. |
PIV FLOW MEASUREMENTS FOR A HIGH LIFT AIRFOIL WITH LEADING EDGE ICE |
ICAS 2008-3.7.4 |
| Goraj, Z. |
MINI UAV DESIGN AND OPTIMIZATION FOR LONG ENDURANCE MISSION |
ICAS 2008-1.5.2 |
| Gore, B. |
CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
| Gore, D. |
LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
| Gorrell, S. |
NUMERICAL INVESTIGATION OF INLET DISTORTION INDUCED SWIRL IN MULTISTAGE FANS |
ICAS 2008-4.4.3 |
| Goulain, M. |
AIRBUS: TOWARDS AN ECO-EFFICIENT ENTERPRISE |
ICAS 2008-4.7.1 INVITED |
| Graff, T. J. |
OPERATIONAL IMPROVEMENTS FROM IN-TRAIL PROCEDURE IN THE NORTH ATLANTIC ORGANIZED TRACK SYSTEM |
ICAS 2008-11.6.1 (AIAA 2008-8898) |
| Graham, M. |
THE MODERNIZED NATIONAL AIRSPACE SYSTEM PERFORMANCE ANALYSIS CAPABILITY (NASPAC) |
ICAS 2008-9.11.2 (AIAA 2008-8945) |
| Granada, S. |
ASSESSMENT OF FLIGHT CREW ACCEPTANCE OF AUTOMATED RESOLUTION SUGGESTIONS AND MANUAL RESOLUTION TOOLS |
ICAS 2008-8.7.2 |
| Grandi, F. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
| Gray, L. |
SIMULTANEOUS IMPROVEMENTS IN ENVIRONMENTAL PERFORMANCE AND OPERATIONAL EFFICIENCY ENABLED BY SIGNIFICANTLY QUIETER AIRCRAFT |
ICAS 2008-11.2.2 (AIAA 2008-8858) |
| Greco Jr., P. C. |
APPLICATION OF A MODEL UPDATING METHOD TO AN AIRCRAFT LONGITUDINAL STABILITY AUGMENTATION SYSTEM |
ICAS2008-5.2 ST: |
| Green, J. |
ICAS - THE FIRST 50 YEARS |
ICAS 2008-0.4 |
| Greenbaum, D. |
METHODOLOGIES FOR ESTIMATING THE IMPACT OF SEVERE WEATHER ON AIRSPACE CAPACITY |
ICAS 2008-10.7.4 (AIAA 2008-8917) |
| Greenberg, J. B. |
PULSATING COMBUSTION OF AN ORGANIC GEL-FUEL DROPLET AND ITS INFLUENCE ON THE THERMAL FIELD OF A SPRAY DIFFUSION FLAME |
ICAS 2008-4.1.2 |
| Greenwell, D. I. |
MODELLING OF STATIC AERODYNAMICS OF HELICOPTER UNDERSLUNG LOADS |
ICAS 2008-5.11.2 |
| Grendysa, W. |
MINI UAV DESIGN AND OPTIMIZATION FOR LONG ENDURANCE MISSION |
ICAS 2008-1.5.2 |
| Grillo, C. |
TRAJECTORY TRACKING FOR A NON - CONVENTIONAL UAV |
ICAS2008-P5.3 |
| Grimaldi, A. |
FE STUDY OF WINDSHIELD SUBJECTED TO HIGH SPEED BIRD IMPACT |
ICAS 2008-9.4.3 |
| Groeneweg, J. |
PILOTED SIMULATION RESULTS OF AN ONBOARD WAKE VORTEX DETECTION, WARNING AND AVOIDANCE SYSTEM AND COCKPIT DISPLAY ASPECTS |
ICAS 2008-9.9.1 |
| Gross, A. |
INVESTIGATION OF SEPARATION CONTROL FOR LOW-PRESSURE TURBINES USING CFD |
ICAS 2008-4.4.2 |
| Grün, G. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
| Grünewald, M. |
MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
| Guardone, A. |
COMPRESSIBLE FLUID-FLOW ALE FORMULATION ON CHANGING TOPOLOGY MESHES FOR AEROELASTIC SIMULATIONS |
ICAS2008-2.10 ST: |
| Guellec, P. |
SYSTEM INFRASTRUCTURE FOR INTEGRATED AND COLLABORATIVE PRODUCT DEVELOPMENT IN THE AERONAUTIC INDUSTRY |
ICAS 2008-6.10.2 |
| Guglieri, G. |
TRAJECTORY OPTIMISATION FOR AUTONOMOUS VEHICLES: A MINIUAV APPLICATION |
ICAS 2008-5.6.3 |
| Guibert, S. |
CONTRACT-BASED AIR TRANSPORTATION SYSTEM TO FULFILL THE ARRIVING-ON-TIME OBJECTIVE |
ICAS 2008-8.2.1 |
| Guichard, L. |
CONTRACT-BASED AIR TRANSPORTATION SYSTEM TO FULFILL THE ARRIVING-ON-TIME OBJECTIVE |
ICAS 2008-8.2.1 |
| Guida, M. |
FE STUDY OF WINDSHIELD SUBJECTED TO HIGH SPEED BIRD IMPACT |
ICAS 2008-9.4.3 |
| Guiler, R. W. |
CONTROL OF A SWEPT WING TAILLESS AIRCRAFT THROUGH WING MORPHING |
ICAS 2008-2.7.1 |
| Guillaume, M. |
UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
| Guillou, Y. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
| Gulding, J. |
THE MODERNIZED NATIONAL AIRSPACE SYSTEM PERFORMANCE ANALYSIS CAPABILITY (NASPAC) |
ICAS 2008-9.11.2 (AIAA 2008-8945) |
| Gunnion, A. J. |
LOADED CARBON COMPOSITE SCARF JOINTS SUBJECT TO QUASI STEADY LATERAL LOADS |
ICAS 2008-7.2.2 |
| Guo, S. |
DEVELOPMENT OF A RUDDERLESS AEROELASTIC FIN TECHNOLOGY |
ICAS 2008-7.10.2 |
| Guo, Y. |
STUDY ON THE RELATIONSHIP BETWEEN CORROSION DAMAGE AND RESIDUAL STRENGTH OF AL 7075-T6 ALLOY |
ICAS 2008-9.8.2 |
| Gupta, A. |
LASER PROPELLED HYPERSONIC AIR-VEHICLE |
ICAS2008-4.3 ST: |
| Gwiggner, C. |
ANALYSIS OF GAPS BETWEEN THE PREDICTIVE AND THE ADAPTIVE COMPONENT IN ATM |
ICAS 2008-11.10.2 (AIAA 2008-8941) |
| György, R. |
POTENTIALS OF LIGHTER-THAN-AIR TECHNOLOGY IN FUTURE MARKETS – AN EVALUATION |
ICAS2008-P1.7 |
| Hahn, K. -U. |
ALLEVIATION OF ATMOSPHERIC FLOW DISTURBANCE EFFECTS ON AIRCRAFT RESPONSE |
ICAS 2008-5.2.2 |
| Haigermoser, C. |
INVESTIGATION OF THE FLOW IN A RECTANGULAR CAVITY USING TOMOGRAPHIC AND TIME-RESOLVED PIV |
ICAS 2008-3.2.2 |
| Haigermoser, C. |
THE EFFECTS OF WALL ROUGHNESS ON THE TURBULENT BOUNDARY LAYER |
ICAS 2008-3.8.1 |
| Hall, K. C. |
REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
| Hallberg, E. |
IHAAA STORE SEPARATION FROM CAVITY (SSC) PROJECT |
ICAS 2008-2.6.2 |
| Hallberg, E. N. |
STORE SEPARATION TRAJECTORY SIMULATION FOR THE HIGH SPEED ANTI-RADIATION DEMONSTRATOR (HSAD) FROM THE F-4 AIRCRAFT |
ICAS 2008-2.9.3 |
| Hallberg, E. N. |
TARGETING POD EFFECTS ON WEAPONS RELEASE FROM THE F-18C HORNET |
ICAS 2008-2.9.4 |
| Halle, W. |
AUGMENTED VISION VIDEOPANORAMA SYSTEM FOR REMOTE AIRPORT TOWER OPERATION |
ICAS 2008-8.3.1 |
| Hammond, D. W. |
A LAYER PAVEMENT MODEL TO SIMULATE ROUGHNESS FEATURES IN ICE ACCRETION NUMERICAL SIMULATION |
ICAS 2008-2.6.1 |
| Han, C. H. |
UNSTEADY PROPULSIVE CHARACTERISTICS OF BIOFOILS MOVING IN A VERY LOW-REYNOLDS NUMBER FLOW |
ICAS 2008-3.9.3 |
| Han, E.-P. |
UTILIZATION OF NETWORK THEORY FOR THE ENHANCEMENT OF ATO AIR ROUTE FORECAST |
ICAS 2008-11.10.5 (AIAA 2008-8944) |
| Han, X. L. |
A FAST GRID DEFORMATION ALGORITHM AND IT’S APPLICATION |
ICAS2008-P2.4 |
| Hansman, R. J. |
ANALYSIS OF INTERACTION BETWEEN AIR TRANSPORTATION AND ECONOMIC ACTIVITY |
ICAS 2008-10.4.2 (AIAA 2008-8888) |
| Hansman, R. J. |
PRELIMINARY ANALYSIS OF STRATEGIES AND CHALLENGES TO ENCOURAGE DATA LINK ADOPTION OVER THE NORTH ATLANTIC AIRSPACE |
ICAS 2008-8.8.3 (AIAA 2008-8953) |
| Hao, L. S. |
RESEARCH ON MONITORING AND CONTROL SYSTEM BASED PLC IN THE NF-6 WIND TUNNEL |
ICAS2008-P2.10 |
| Haraldsdottir, A. |
ANALYSIS OF ARRIVAL MANAGEMENT PERFORMANCE WITH AIRCRAFT REQUIRED TIME OF ARRIVAL CAPABILITIES |
ICAS 2008-11.9.3 (AIAA 2008-8932) |
| Hardy, P. |
A NOVEL RECIPROCAL SOUND TRANSMISSION MEASURING METHOD, APPLIED ON A COMPOSITE FUSELAGE |
ICAS 2008-4.9.3 |
| Harris, D. |
DESIGN OF EXPERIMENT FOR THE PILOT EVALUATION OF AN AIRBORNE RUNWAY INCURSION ALERTING SYSTEM |
ICAS 2008-9.10.2 |
| Hartung, D. |
MECHANICS OF COMPOSITES IN LIGHTWEIGHT STRUCTURES: EFFICIENT TESTING AND COMPUTATION ACCOUNTING FOR COMPLEX 3D BEHAVIOUR |
ICAS 2008-7.11.2 |
| Hashimoto, J. -I. |
CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION |
ICAS 2008-1.2.3 |
| Hatanaka, K. |
MULTI-DISCIPLINARY DESIGN EXPLORATION FOR WINGLET |
ICAS 2008-1.1.3 |
| Haucke, F. |
ACTIVE SEPARATION CONTROL ON A SLATLESS 2D HIGH-LIFT WING SECTION |
ICAS 2008-3.11.2 |
| Hauf, T. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
| Haupt, M. C. |
NUMERICAL ANALYSIS OF THIN-WALLED STRUCTURES IN HYPERSONIC FLOW REGIME |
ICAS 2008-3.6.1 |
| Haupt, M. C. |
NUMERICAL SIMULATION OF AN OSCILLATING AND FLEXIBLE AIRFOIL FOR FLAPPING WING PROPULSION WITH FLUID-STRUCTURE INTERACTION |
ICAS 2008-7.10.4 |
| Hayase, T. |
MEASUREMENT OF UNSTEADY AERODYNAMIC FORCES OF 3D FLAPPING WING IN HOVERING TO FORWARD FLIGHT |
ICAS 2008-3.4.3 |
| Heatley, D. P |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
| Heblij, S. J. |
OPTIMIZATION OF RNAV NOISE ABATEMENT ARRIVAL TRAJECTORIES |
ICAS 2008-4.11.1 |
| Heere,, K. |
ALGORITHM AND OPERATIONAL CONCEPT FOR RESOLVING SHORT-RANGE CONFLICTS |
ICAS 2008-8.7.5 |
| Heiligers, M. M. |
FEASIBILITY ANALYSIS OF ACHIEVING A STABILIZED APPROACH |
ICAS 2008-5.4.2 |
| Heinze, W. |
THE GREEN FREIGHTER PROJECT - OBJECTIVES AND FIRST RESULTS |
ICAS 2008-4.10.3 |
| Hellbach, T. |
TOWARDS SESAR PERFORMANCE TARGETS - THE SUPER-HIGHWAY APPROACH |
ICAS 2008-10.10.1 (AIAA 2008-8935) |
| Hendrick, P. |
A FLIGHT THRUST DECK FOR THE F100 TURBOFAN OF THE F16 AIRCRAFT |
ICAS 2008-4.5.1 |
| Hendrick, P. |
PRELIMINARY DESIGN OF A JOINED WING HALE UAV |
ICAS 2008-1.4.3 |
| Henke, R. |
LONG TERM AIRCRAFT PROJECT AND TECHNOLOGY EVALUATION UNDER THE UNCERTAINTY OF FUTURE SCENARIOS |
ICAS 2008-1.3.4 |
| Herbiet, J. -F. |
A FLIGHT THRUST DECK FOR THE F100 TURBOFAN OF THE F16 AIRCRAFT |
ICAS 2008-4.5.1 |
| Herbin, E. |
UNCERTAINTIES AT THE CONCEPTUAL STAGE: MULTILEVEL MULTIDISCIPLINARY DESIGN AND OPTIMIZATION APPROACH |
ICAS 2008-1.1.2 |
| Hering, H. |
FROM ANALOGUE BROADCAST RADIO TOWARDS END-TO-END COMMUNICATION |
ICAS2008-P8.3 (AIAA 2008-8874) |
| Heringer, F. M. |
580 A MULTIDISCIPLINARY OPTIMIZATION METHOD APPLIED TO AIRCRAFT DESIGN |
ICAS2008-P1.4 |
| Hernandez, S. |
SIZE OPTIMIZATION OF AIRCRAFT STRUCTURES |
ICAS2008-7.11 ST: |
| Hernández, S. |
THERMAL DESIGN UNDER UNCERTAINTIES OF AIRCRAFT STRUCTURES |
ICAS 2008-7.2.3 |
| Herreria, J. A. |
SAFE AUTOMATIC FLIGHT BACK AND LANDING OF AIRCRAFT (SOFIA) |
ICAS2008-9.7 ST: |
| Herszberg, I. |
LOADED CARBON COMPOSITE SCARF JOINTS SUBJECT TO QUASI STEADY LATERAL LOADS |
ICAS 2008-7.2.2 |
| Hess, D. E. |
SIMULATION OF A NON-AXISYMMETRIC UNDERSEA VEHICLE USING A RECURSIVE NEURAL NETWORK |
ICAS 2008-5.8.2 |
| Hesselink, H. H. |
ENVIRONMENT-AWARE RUNWAY ALLOCATION ADVICE SYSTEM |
ICAS 2008-4.11.2 |
| Hiernaux, O. |
EVOLUTION OF FUTURE EQUIPMENTS AND SUB-SYSTEMS FOR THE FUTURE GREEN AIRCRAFT |
ICAS 2008-6.4.1 INVITED |
| Higuchi, K. |
WING DESIGN OF SUPERSONIC TRANSPORT BY A MULTI-POINT OPTIMIZATION METHOD |
ICAS 2008-2.4.3 |
| Hileman, J. I. |
PAYLOAD FUEL ENERGY EFFICIENCY AS A METRIC FOR AVIATION ENVIRONMENTAL PERFORMANCE |
ICAS 2008-4.7.4 |
| Hileman, J. I. |
THE FEASIBILITY AND POTENTIAL ENVIRONMENTAL BENEFITS OF ALTERNATIVE FUELS FOR COMMERCIAL AVIATION |
ICAS 2008-4.7.5 |
| Hirai, K. |
VORTEX BEHAVIORS OF CRANKED ARROW WING CONFIGURATIONS WITH DIFFERENT WING PLANFORMS |
ICAS 2008-3.3.2 |
| Hirai, T. |
OVERVIEW OF THE NUMERICAL SIMULATIONS OF THE HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL |
ICAS2008-2.2 ST: |
| Hitzel, M. |
AERODYNAMIC OPTIMIZATION OF AIRCRAFT CONFIGURATIONS WITH MULTIDISZIPLINARY ASPECTS |
ICAS 2008-2.11.3 |
| Hiyama, J. |
HIGH-ORDER LARGE EDDY SIMULATION AROUND 2-D AEROFOIL WITH HIGH-LIFT DEVICE |
ICAS 2008-2.1.2 |
| Hochstetler, R. |
AIRSHIP TRANSPORT OPERATIONAL MANAGEMENT IN NORTHERN LATITUDES |
ICAS 2008-10.1.1 (AIAA 2008-8850) |
| Höcht, L. |
TRAJECTORY CONTROL IMPROVEMENT BASED ON A NONLINEAR DYNAMIC INVERSION APPROACH |
ICAS 2008-5.7.2 |
| Hoeijmakers, H. W. M. |
NUMERICAL SIMULATION OF ICE ACCRETION ON MULTIPLE-ELEMENT AIRFOIL SECTIONS |
ICAS 2008-2.2.2 |
| Hofbauer, K. |
FROM ANALOGUE BROADCAST RADIO TOWARDS END-TO-END COMMUNICATION |
ICAS2008-P8.3 (AIAA 2008-8874) |
| Hofbauer, W. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
| Hoffman, J. |
AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
| Hoffman, R. |
CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
| Hoffman, R. |
PRINCIPLES OF AIRSPACE TUBE DESIGN FOR DYNAMIC AIRSPACE CONFIGURATION |
ICAS 2008-10.10.5 (AIAA 2008-8939) |
| Hogenhuis, R. H. |
A PRACTICAL APPROACH TO MULTI-OBJECTIVE CAPACITY ANALYSIS OF AN ENVIRONMENT-AWARE AIRPORT |
ICAS 2008-8.5.1 |
| Hogenhuis, R. H. |
OPTIMIZATION OF RNAV NOISE ABATEMENT ARRIVAL TRAJECTORIES |
ICAS 2008-4.11.1 |
| Holden, T. |
AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
| Hollingsworth, P. |
A METHOD FOR ASSESSING THE ENVIRONMENTAL BENEFIT OF FUTURE AVIATION TECHNOLOGIES |
ICAS2008-P10.2 |
| Holm, A. H. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
| Holmberg, A. |
ROUTE PLANNING FOR RELAY UAV |
ICAS 2008-5.6.2 |
| Holmes, B. J. |
IMPLEMENTING NEXT GENERATION AIR TRANSPORTATION SYSTEM TECHNOLOGIES |
ICAS 2008-8.4.3 |
| Holsclaw, C. |
GOING GREEN – MITIGATING AVIATION’S NEW ENVIRONMENTAL DRIVERS |
ICAS 2008-4.7.2 |
| Holzapfel, F. |
IMPROVEMENT FOR LANDING ON SMALL-MEDIUM AIRPORTS USING FUTURE, AIRCRAFT-AUTONOMOUS GUIDANCE AIDS |
ICAS 2008-5.7.1 INVITED |
| Holzapfel, F. |
TRAJECTORY CONTROL IMPROVEMENT BASED ON A NONLINEAR DYNAMIC INVERSION APPROACH |
ICAS 2008-5.7.2 |
| Holzapfel, F. |
UNIQUE PERFORMANCE CHARACTERISTICS OF SOLAR AIRCRAFT |
ICAS 2008-5.3.2 |
| Holzäpfel, F. |
AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION FOR TAKE-OFF AND DEPARTURE |
ICAS 2008-11.8.3 (AIAA 2008-8921) |
| Holzäpfel, F. |
PERFORMANCE OF THE WAKE VORTEX PREDICTION AND MONITORING SYSTEM WSVBS AT FRANKFURT AIRPORT |
ICAS 2008-8.11.2 |
| Holzwarth, R. |
FLIGHT VEHICLE COMPOSITE STRUCTURES |
ICAS 2008-7.9.1 (AIAA 2008-8976 ) |
| Homan, J. J. |
THE INFLUENCE OF FATIGUE CRACK INITIATION BEHAVIOUR OF FRICTION STIR WELDED JOINTS ON THE DESIGN CRITERIA |
ICAS 2008-7.6.2 |
| Homola, J. |
HUMAN-IN-THE-LOOP EVALUATION OF GROUND-BASED AUTOMATED SEPARATION ASSURANCE FOR NEXTGEN |
ICAS 2008-11.4.5 (AIAA 2008-8885) |
| Hong, S.- M. |
15 THE SIGNAL-TO-NOISE RATIO MODELING OF RADAR IN ELECTRONIC COUNTER-COUNTER MEASURES |
ICAS2008-P6.7 |
| Hoogendijk, P. L. |
MULTI-DISCIPLINARY INSTALLATION OF THE EAGLE'S EYE |
ICAS2008-P6.9 |
| Hook, L. R. |
147 THE LOW DOWN – DIGITAL TERRAIN DATA FOR AUTOMATIC GROUND COLLISION AVOIDANCE |
ICAS2008-P6.10 |
| Horinouchi, S. |
NOISE REDUCTION BY THRUST VECTORING FOR SUPERSONIC BUSINESS JET |
ICAS 2008-4.8.3 |
| Horn, W. |
"ACTIVE CORE" - A KEY TECHNOLOGY FOR MORE ENVIRONMENTALLY FRIENDLY AERO ENGINES BEING INVESTIGATED UNDER THE NEWAC PROGRAM |
ICAS 2008-4.2.1 |
| Horst, P. |
NUMERICAL ANALYSIS OF THIN-WALLED STRUCTURES IN HYPERSONIC FLOW REGIME |
ICAS 2008-3.6.1 |
| Horst, P. |
NUMERICAL SIMULATION OF AN OSCILLATING AND FLEXIBLE AIRFOIL FOR FLAPPING WING PROPULSION WITH FLUID-STRUCTURE INTERACTION |
ICAS 2008-7.10.4 |
| Horton, G. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
| Hoseinalipour, S. M. |
EXPERIMENTAL INVESTIGATION OF SPRAY CHARACTERISTICS OF DOUBLE-BASE SWIRL INJECTOR |
ICAS2008-4.1 ST: |
| Hospers, J. M. |
NUMERICAL SIMULATION OF ICE ACCRETION ON MULTIPLE-ELEMENT AIRFOIL SECTIONS |
ICAS 2008-2.2.2 |
| Howell, D. |
OPERATIONAL ASSESSMENT OF THE INTEGRATED TERMINAL WEATHER SYSTEM (ITWS) USING DIRECT MEASUREMENT |
ICAS 2008-10.7.5 (AIAA 2008-8918) |
| Howell, K. M. |
LARGE UAS OPERATIONS IN THE NAS - THE NASA 2007 WESTERN STATES FIRE MISSIONS |
ICAS 2008-8.1.3 (AIAA 2008-8967) |
| Howland, M. |
AIRSPACE SECURITY MEASURES EMPLOYED FOR THE UN GENERAL ASSEMBLY MEETING: ANALYSIS AND IMPACT |
ICAS 2008-11.5.1 (AIAA 2008-8892) |
| Hsieh, C. H. |
THE IMPLEMENTATION OF ANALYTICAL HIERARCHY PROCESS IN FLIGHT SAFETY |
ICAS 2008-9.2.4 |
| Hu, Y. F. |
METHODS FOR CALCULATING THE DAMAGE-RATE OF AIRCRAFT COMPONENT |
ICAS2008-9.8 ST: |
| Huang, C. K. |
NUMERICAL SIMULATION OF FLAPPING WING AERODYNAMIC PERFORMANCE UNDER GUST WIND CONDITIONS |
ICAS2008-3.5 ST: |
| Huang, P. |
ANALYSIS OF THE SCATTERING CHARACTERISTICS FROM DISCONTINUITY SURFACES ON AIRCRAFT USING A MODIFIED MLFMA |
ICAS2008-P3.6 |
| Huang, X. |
SUPPRESSING BOUNDARY LAYER SEPARATION BY UNSTEADY EXCITATION OF MINI-SCALE LEADING-EDGE FLAPS |
ICAS 2008-3.10.1 |
| Huber, C. |
STATIC AND FATIGUE ANALYSIS OF AN UPPER WING SKIN WITH EXFOLIATION CORROSION |
ICAS 2008-7.4.1 |
| Hübner, N. |
PREPARING LP TURBINE TECHNOLOGY FOR MODERN AIRCRAFT ENGINES |
ICAS 2008-4.6.1 |
| Huebsch, W. W. |
CONTROL OF A SWEPT WING TAILLESS AIRCRAFT THROUGH WING MORPHING |
ICAS 2008-2.7.1 |
| Hui, K. |
CESSNA CITATION CJ1 FLIGHT TEST DATA GATHERING AND LEVEL-C SIMULATOR MODEL DEVELOPMENT |
ICAS 2008-5.1.2 |
| Hummel, D. |
THE SECOND INTERNATIONAL VORTEX FLOW EXPERIMENT (VFE-2): RESULTS OF THE FIRST PHASE 2003 - 2008 |
ICAS 2008-3.3.1 INVITED |
| Hunter, G. |
TOWARD AN ECONOMIC MODEL TO INCENTIVIZE VOLUNTARY OPTIMIZATION OF NAS TRAFFIC FLOW |
ICAS 2008-10.4.1 (AIAA 2008-8887) |
| Hüttig, G. |
RESEARCH ON INTEGRATED COLLIMATED COCKPIT VISUAL AND FLIGHT INFORMATION SYSTEM |
ICAS 2008-9.10.1 |
| Huysseune, J. |
EVOLUTION OF FUTURE EQUIPMENTS AND SUB-SYSTEMS FOR THE FUTURE GREEN AIRCRAFT |
ICAS 2008-6.4.1 INVITED |
| Hwang, T. W |
NONLINEAR FORMATION GUIDANCE LAW WITH ROBUST DISTURBANCE OBSERVER |
ICAS 2008-5.7.4 |
| Hwang, T. W. |
INTEGRATED INTERCEPT MISSILE GUIDANCE AND CONTROL WITH TERMINAL ANGLE CONSTRAINT |
ICAS 2008-5.7.3 |
| Ichikawa, G. |
ESTIMATION OF THE INFLUENCE OF PROFILE ERROR ON AERODYNAMIC PERFORMANCE FOR LOW-REYNOLDS-NUMBER AIRFOILS |
ICAS2008-3.7 ST: |
| Idris, H. |
TASK ANALYSIS FOR FEASIBILITY ASSESSMENT OF A COLLABORATIVE TRAFFIC FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.7.3 (AIAA 2008-8909) |
| Iijima, T. |
CBAQ: DEVELOPMENT OF CRM BEHAVIOR ANALYSIS METHOD FOR MISSION FLIGHT CREW TRAINING |
ICAS 2008-9.2.1 |
| Ikeda, T. |
INTERFACE CONDITIONS OF FINITE-DIFFERENCE COMPACT SCHEMES FOR COMPUTATIONAL AEROACOUSTICS |
ICAS 2008-2.3.1 |
| Imamura, T. |
OVERVIEW OF THE NUMERICAL SIMULATIONS OF THE HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL |
ICAS2008-2.2 ST: |
| Inokuchi, H. |
DEVELOPMENT OF AN ONBOARD DOPPLER LIDAR FOR FLIGHT SAFETY |
ICAS 2008-9.9.2 |
| Irving, P. E. |
SIMPLIFYING MSD MODELING BY USING CONTINUING DAMAGE ASSUMPTION AND PARAMETRIC STUDY: THE ROLE OF RIVET SQUEEZE FORCE |
ICAS 2008-9.8.1 |
| Isaksson, O. |
VIRTUAL ENTERPRISE COLLABORATION - BREAKTHROUGH TECHNOLOGIES PROVIDED BY VIVACE |
ICAS 2008-8.10.4 INVITED |
| Iscold, P. H. A. O. |
DEVELOPMENT OF A SMALL UNMANNED AIR VEHICLE WITH MINIMUM SENSORS PHILOSOPHY |
ICAS2008-1.4 ST: |
| Ishikawa, H. |
FLIGHT TEST RESULTS AT TRANSONIC REGION ON SUPERSONIC EXPERIMENTAL AIRPLANE (NEXST-1) |
ICAS 2008-2.4.2 |
| Ishikawa, H. |
NUMERICAL STUDY OF A PITOT PROBE WITH FIVE-HOLE PYRAMIDAL HEAD FOR SUPERSONIC FLIGHT TEST |
ICAS 2008-3.2.4 |
| Ishutkina, M. A. |
ANALYSIS OF INTERACTION BETWEEN AIR TRANSPORTATION AND ECONOMIC ACTIVITY |
ICAS 2008-10.4.2 (AIAA 2008-8888) |
| Isikveren, A. T. |
DEVELOPMENT AND VALIDATION OF A NEXT-GENERATION CONCEPTUAL AERO-STRUCTURAL SIZING SUITE |
ICAS 2008-1.6.2 |
| Isogai, K. |
MEASUREMENT OF UNSTEADY AERODYNAMIC FORCES OF 3D FLAPPING WING IN HOVERING TO FORWARD FLIGHT |
ICAS 2008-3.4.3 |
| Isogai, K. |
OPTIMUM AEROELASTIC DESIGN OF A RESONANCE TYPE FLAPPING WING FOR MICRO AIR VEHICLES |
ICAS 2008-7.10.3 |
| Israeli, E. R. |
COMPUTATIONAL INVESTIGATION AND DESIGN OF COMPLIANT MEMBRANE WINGS FOR BIOLOGICALLY INSPIRED FLIGHT VEHICLES |
ICAS 2008-2.10.1 |
| Ito, K. |
PARAMETRIC STUDY AND MITIGATION OF PORPOISING IN WATERBORN AIRCRAFTS |
ICAS2008-5.8 ST: |
| Ito, T. |
AEROACOUSTIC NOISE MEASUREMENTS IN AERODYNAMIC LOW-SPEED WIND TUNNELS |
ICAS 2008-3.2.3 |
| Ito, T. |
COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA |
ICAS 2008-2.2.1 |
| Ito, T. |
INVESTIGATION OF THE FLOW OVER NACELLE/PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION |
ICAS 2008-3.3.3 |
| Itoh, E. |
HARMONIZING AUTOMATION, PILOT AND AIR TRAFFIC CONTROLLER IN THE FUTURE AIR TRAFFIC MANAGEMENT |
ICAS 2008-8.2.4 |
| Iuso, G. |
LARGE-SCALE MANIPULATION OF A TURBULENT BOUNDARY LAYER BY MEANS OF A 2D SYNTHETIC JET |
ICAS2008-P2.8 |
| Iuso, G. |
TRANSVERSAL INJECTED SYNTHETIC JETS FOR WALL TURBULENCE CONTROL |
ICAS 2008-3.10.3 |
| Ivanov, M. J. |
UNSTEADY CFD MODELING OF WHOLE GAS TURBINE ENGINE FLOW PASSAGE WITH APPLICATIONS |
ICAS2008-4.4 ST: |
| Jacazio, G. |
A DUAL-DUPLEX ELECTROHYDRAULIC SYSTEM FOR THE FLY-BY-WIRE CONTROL OF A HELICOPTER MAIN ROTOR |
ICAS 2008-6.6.4 |
| Jackson, C. |
METHODOLOGIES FOR ESTIMATING THE IMPACT OF SEVERE WEATHER ON AIRSPACE CAPACITY |
ICAS 2008-10.7.4 (AIAA 2008-8917) |
| Jacobs, S. J. |
NUMERICAL SIMULATION OF ICE ACCRETION ON MULTIPLE-ELEMENT AIRFOIL SECTIONS |
ICAS 2008-2.2.2 |
| Jaenker, P. |
PIEZO ACTIVE VIBRATION AND NOISE CONTROL IN HELICOPTERS |
ICAS 2008-4.9.2 INVITED |
| Jafari, A. A. |
SCALED DOWN MODELS FOR FREE VIBRATION ANALYSIS OF ORTHOGONALLY STIFFENED CYLINDRICAL SHELLS USING SIMILITUDE THEORY |
ICAS 2008-7.7.5 |
| Jahagirdar, Y. P. |
DESIGN, FABRICATION AND OPERATION OF REMOTELY CONTROLLED AIRSHIPS IN INDIA |
ICAS 2008-10.1.3 (AIAA 2008-8853) |
| Jahangir, E. |
SIMULTANEOUS IMPROVEMENTS IN ENVIRONMENTAL PERFORMANCE AND OPERATIONAL EFFICIENCY ENABLED BY SIGNIFICANTLY QUIETER AIRCRAFT |
ICAS 2008-11.2.2 (AIAA 2008-8858) |
| Jatiningrum, D. |
648 TEST FLYING UNMANNED WISE AS A MEANS FOR PROOF OF CONCEPT |
ICAS2008-P5.7 |
| Jenie, S.D. |
648 TEST FLYING UNMANNED WISE AS A MEANS FOR PROOF OF CONCEPT |
ICAS2008-P5.7 |
| Jenks, M. |
THE BOEING 787 DREAMLINER PROGRAMME |
ICAS 2008-0.8 |
| Jeon, K. -S. |
A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
| Jia, X. H. |
CFD RESEARCH FOR AIR-TO-AIR MISSILE WITH LATERAL JET CONTROL |
ICAS2008-2.64 ST: |
| Jimenez, H. |
TECHNOLOGY-ENABLED IMPROVEMENTS FOR TERMINAL AREA CAPACITY AND ENVIRONMENTAL IMPACT |
ICAS 2008-4.11.3 |
| Jin, Y. |
AUTOMATED ASSEMBLY TIME ANALYSIS USING A DIGITAL KNOWLEDGE BASED APPROACH |
ICAS 2008-10.3.1 (AIAA 2008-8861) |
| Johansson, T. G |
EVALUATION OF THE FLOW IN AN INTERMEDIATE TURBINE DUCT AT OFF-DESIGN CONDITIONS |
ICAS 2008-4.6.2 |
| Johnson, E. |
POTENTIAL ACTIVE-VISION CONTROL SYSTEMS FOR UNMANNED AIRCRAFT |
ICAS 2008-6.8.2 INVITED |
| Johnson, N. |
ASSESSMENT OF FLIGHT CREW ACCEPTANCE OF AUTOMATED RESOLUTION SUGGESTIONS AND MANUAL RESOLUTION TOOLS |
ICAS 2008-8.7.2 |
| Johnson, W. J. |
ASSESSMENT OF FLIGHT CREW ACCEPTANCE OF AUTOMATED RESOLUTION SUGGESTIONS AND MANUAL RESOLUTION TOOLS |
ICAS 2008-8.7.2 |
| Johnston, R. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
| Jonas, M. |
MINI UAV DESIGN AND OPTIMIZATION FOR LONG ENDURANCE MISSION |
ICAS 2008-1.5.2 |
| Jones, J. |
DESIGN FOR PROCESS EXCELLENCE - ENSURING TIMELY AND COST EFFECTIVE SOLUTIONS |
ICAS 2008-6.7.4 |
| Jones, K. M. |
OPERATIONAL IMPROVEMENTS FROM IN-TRAIL PROCEDURE IN THE NORTH ATLANTIC ORGANIZED TRACK SYSTEM |
ICAS 2008-11.6.1 (AIAA 2008-8898) |
| Jones, K. M. |
PILOT IN-TRAIL PROCEDURE VALIDATION SIMULATION STUDY |
ICAS 2008-10.5.2 (AIAA 2008-8896) |
| Jouaillec, F. |
THE REGIONAL AEROSPACE CLUSTER POLICY IN EUROPE |
ICAS 2008-6.9.2 |
| Jouannet, C. |
AIRCRAFT CONCEPTUAL DESIGN AUTOMATION |
ICAS 2008-1.8.1 |
| Joulia, A. |
INNOVATIVE FUTURE AIR TRANSPORT SYSTEM: SIMULATION OF A FULLY AUTOMATED ATS |
ICAS 2008-8.4.5 |
| Judas, M. |
MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
| Juhász, A. |
FEASIBILITY STUDY ON MULTI-PHASE FLOW SIMULATION OF FUEL INJECTION USING LATTICE BOLTZMANN METHOD |
ICAS 2008-4.3.4 |
| Jump, M. |
BIOMECHANICAL PILOT PROPERTIES IDENTIFICATION BY INVERSE KINEMATICS/INVERSE DYNAMICS MULTIBODY ANALYSIS |
ICAS 2008-9.10.4 |
| Jung, Y. |
AN OPTIMIZATION MODEL FOR REDUCING AIRCRAFT TAXI TIMES AT THE DALLAS-FORT WORTH INTERNATIONAL AIRPORT |
ICAS 2008-8.6.1 |
| Jung, Y. |
IMPLICATION OF VARIABILITY IN AIRPORT SURFACE OPERATIONS ON 4-D TRAJECTORY PLANNING |
ICAS 2008-11.11.3 (AIAA 2008-8960) |
| Jung, Y. |
IMPROVED PREDICTION OF GATE DEPARTURE TIMES USING PRE-DEPARTURE EVENTS |
ICAS 2008-11.8.1 (AIAA 2008-8919) |
| Kageyama, K. |
DESIGN OF OPERATION DATABASE FOR ATM PERFORMANCE ASSESSMENT |
ICAS 2008-8.9.4 |
| Kalnins, K. |
METAMODELS FOR THE OPTIMIZATION OF DAMAGE-TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.3.3 |
| Kaltenhäuser, S. |
REAL TIME SIMULATION OF INTEGRATION OF UAV'S INTO AIRSPACE |
ICAS 2008-8.1.1 |
| Kamisawa, Y. |
OPTIMUM AEROELASTIC DESIGN OF A RESONANCE TYPE FLAPPING WING FOR MICRO AIR VEHICLES |
ICAS 2008-7.10.3 |
| Kamiyoshihara, Y. |
DEVELOPMENT OF THE DISPLAY DEVICE OF POWER DISTIBUTION SYSTEM (DEVELOPMENT OF THE DEPTH FUSED 3-D DISPLAY FOR AIRCRAFT) |
ICAS2008-6.5 ST: |
| Kanazaki, M. |
INVESTIGATION OF THE FLOW OVER NACELLE/PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION |
ICAS 2008-3.3.3 |
| Kang, R. |
THE SYSTEM FAULT BEHAVIOR AND MODEL |
ICAS2008-P9.2 |
| Karama, M. |
RELIABILITY STUDY OF POWER MODULE BY STOCHASTIC UNCERTAINTY METHOD FOR AN AERONAUTICAL APPLICATION |
ICAS 2008-6.1.1 |
| Kargar Neghab, A. |
EXPERIMENTAL INVESTIGATION OF SPRAY CHARACTERISTICS OF DOUBLE-BASE SWIRL INJECTOR |
ICAS2008-4.1 ST: |
| Karl, A. |
DESIGN FOR PROCESS EXCELLENCE - ENSURING TIMELY AND COST EFFECTIVE SOLUTIONS |
ICAS 2008-6.7.4 |
| Kasai, K. |
ESTIMATION OF THE INFLUENCE OF PROFILE ERROR ON AERODYNAMIC PERFORMANCE FOR LOW-REYNOLDS-NUMBER AIRFOILS |
ICAS2008-3.7 ST: |
| Kato, H. |
COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA |
ICAS 2008-2.2.1 |
| Kato, H. |
INVESTIGATION OF THE FLOW OVER NACELLE/PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION |
ICAS 2008-3.3.3 |
| Kato, T. |
RELATION BETWEEN TRAILING EDGE NOISE AND BOUNDARY LAYER INSTABILITY |
ICAS2008-P2.14 |
| Katz, J. B. |
PAYLOAD FUEL ENERGY EFFICIENCY AS A METRIC FOR AVIATION ENVIRONMENTAL PERFORMANCE |
ICAS 2008-4.7.4 |
| Katzenberger, K.W. |
F/A 18 E/F TOTAL PRODUCTION SYSTEM |
ICAS 2008-6.7.2 |
| Kawadu, T. |
DEVELOPMENT OF THE DISPLAY DEVICE OF POWER DISTIBUTION SYSTEM (DEVELOPMENT OF THE DEPTH FUSED 3-D DISPLAY FOR AIRCRAFT) |
ICAS2008-6.5 ST: |
| Kawai, M. |
AERODYNAMIC DESIGN AND ITS VALIDATION OF AN OPEN-TYPE ENGINE RUN-UP FACILITY |
ICAS 2008-4.5.3 |
| Kawazoe, H. |
FOREBODY VORTEX CONTROL ON HIGH PERFORMANCE AIRCRAFT USING PWM-CONTROLLED PLASMA ACTUATORS |
ICAS 2008-3.3.4 |
| Keck, B. |
REAL TIME SIMULATION OF INTEGRATION OF UAV'S INTO AIRSPACE |
ICAS 2008-8.1.1 |
| Kelly, P. |
AEROSPACE PRODUCT COST MANAGEMENT AT THE EARLY CONCEPT OPERATIONS PHASE |
ICAS 2008-10.6.2 (AIAA 2008-8904) |
| Kennepohl, F. |
PREPARING LP TURBINE TECHNOLOGY FOR MODERN AIRCRAFT ENGINES |
ICAS 2008-4.6.1 |
| Kerns, K. |
SAY WHO? PILOTED SIMULATION STUDY OF COMMUNICATIONS CENTERED AROUND A COCKPIT TRAFFIC DISPLAY |
ICAS 2008-10.5.1 (AIAA 2008-8895) |
| Khalid, M. |
A CFD STUDY OF UCAV 1303 BASELINE MODEL AT CRUISE MACH NUMBERS |
ICAS 2008-2.5.1 |
| Khan, S. U. |
FATIGUE CRACK GROWTH PREDICTION OF FIBRE REINFORCED METAL LAMINATES UNDER VARIABLE AMPLITUDE LOADING |
ICAS 2008-7.6.1 |
| Khan, Z. |
MECHANICALLY UNCOUPLED SERVO TABS FOR PRIMARY FLIGHT CONTROLS |
ICAS 2008-5.2.3 |
| Khodagolian, V. |
AERODYNAMIC STALL SUPPRESSION ON AEROFOIL SECTIONS USING PASSIVE AIR JET VORTEX GENERATORS |
ICAS 2008-3.11.3 |
| Khosoussi, S. |
FEM MICRO-MECHANICAL ANALYSIS OF DELAMINATION PHENOMENON IN IMC LAMINATED COMPOSITES USING DAMAGE THEORY |
ICAS2008-9.4 ST: |
| Khreish, J. |
EVALUATION OF AN INTEROPERABLE VERTICAL TAKE-OFF UAV FOR OPERATIONS WITH UGVS - AN OVERVIEW |
ICAS 2008-6.11.2 |
| Khromov, V. |
GROUND EFFECT MODELING FOR ROTARY-WING SIMULATION |
ICAS 2008-5.11.3 |
| Khurana, M. S. |
APPLICATION OF AN HYBRID OPTIMIZATION APPROACH IN THE DESIGN OF LONG ENDURANCE AIRFOILS |
ICAS 2008-2.8.2 |
| Kielb, R. E. |
REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
| Kim, B. |
SIMULTANEOUS IMPROVEMENTS IN ENVIRONMENTAL PERFORMANCE AND OPERATIONAL EFFICIENCY ENABLED BY SIGNIFICANTLY QUIETER AIRCRAFT |
ICAS 2008-11.2.2 (AIAA 2008-8858) |
| Kim, B. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
| Kim, B. J. |
PERFORMANCE EVALUATION AND HILS TEST OF CONTROL ALLOCATION METHODS FOR RECONFIGURATION CONTROL |
ICAS 2008-5.10.3 |
| Kim, E. T. |
PERFORMANCE EVALUATION AND HILS TEST OF CONTROL ALLOCATION METHODS FOR RECONFIGURATION CONTROL |
ICAS 2008-5.10.3 |
| Kim, J. |
TRAJECTORY UNCERTAINTY MODELING FOR QUEUEING ANALYSIS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.1.1 (AIAA 2008-8854) |
| Kim, M. |
BIRD-STRIKE DAMAGE ANALYSIS IN CONCEPT ADVANCED COMPOSITE FAN BLADES |
ICAS 2008-4.4.1 |
| Kim, S. |
A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
| Kim, T. H |
NONLINEAR FORMATION GUIDANCE LAW WITH ROBUST DISTURBANCE OBSERVER |
ICAS 2008-5.7.4 |
| Kim, Y. S. |
OPTIMIZATION FOR FLIGHT CONTROL SYSTEM WITH CONSTRAINTS SUPPLEMENTED HANDLING QUALITIES |
ICAS 2008-5.3.4 |
| King, J. |
ANALYSIS OF ARRIVAL MANAGEMENT PERFORMANCE WITH AIRCRAFT REQUIRED TIME OF ARRIVAL CAPABILITIES |
ICAS 2008-11.9.3 (AIAA 2008-8932) |
| Kintscher, M. |
ACTIVE AND PASSIVE STRUCTURAL MEASURES FOR AEROELASTIC WINGLET DESIGN |
ICAS 2008-7.10.1 |
| Kirby, M. R. |
AN APPROACH FOR VERIFICATION AND VALIDATION OF THE ENVIRONMENTAL DESIGN SPACE |
ICAS2008-P8.4 (AIAA 2008-8875) |
| Kirby, M. R. |
THE ENVIRONMENTAL DESIGN SPACE |
ICAS 2008-4.7.3 |
| Kladetzke, J. |
AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION FOR TAKE-OFF AND DEPARTURE |
ICAS 2008-11.8.3 (AIAA 2008-8921) |
| Klar, J. U. |
FIN BUFFET CHARACTERISTICS OF ADVANCED TRAINER AIRCRAFT |
ICAS 2008-3.4.1 |
| Kling, A. |
COLLAPSE BEHAVIOR OF THIN-WALLED CFRP STRUCTURES DUE TO MATERIAL AND GEOMETRIC NONLINEARITIES–EXPERIMENTS AND SIMULATION |
ICAS 2008-7.11.3 |
| Klingauf, U. |
SIMULATOR EVALUATION OF A NOVEL SURFACE MOVEMENT AWARENESS AND ALERTING SYSTEM (SMAAS) FOR RUNWAY INCURSION AVOIDANCE |
ICAS 2008-11.11.2 (AIAA 2008-8959) |
| Kloepperl, V. |
PIEZO ACTIVE VIBRATION AND NOISE CONTROL IN HELICOPTERS |
ICAS 2008-4.9.2 INVITED |
| Knoerzer, D. |
EUROPE'S RESEARCH TACKLES THE GLOBAL CHALLENGES TO AERONAUTICS |
ICAS 2008-6.9.1 INVITED |
| Koenig, R. |
DESIGN OF 4D LANDING APPROACH TRAJECTORIES FOR A QUIET STOL AIRPLANE |
ICAS 2008-4.8.2 |
| Koenig, R. |
EVALUATION OF SIMULATOR AND FLIGHT TESTED NOISE ABATEMENT APPROACH PROCEDURES |
ICAS 2008-4.8.1 |
| Koenke, E. |
DEVELOPMENT AND APPLICATION OF AN INTEGRATED APPROACH TOWARD NASA AIRSPACE SYSTEMS RESEARCH |
ICAS 2008-10.8.1 (AIAA 2008-8924) |
| Koepf, A. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
| Kohama, Y. |
RELATION BETWEEN TRAILING EDGE NOISE AND BOUNDARY LAYER INSTABILITY |
ICAS2008-P2.14 |
| Kokkalis, A. |
AERODYNAMIC STALL SUPPRESSION ON AEROFOIL SECTIONS USING PASSIVE AIR JET VORTEX GENERATORS |
ICAS 2008-3.11.3 |
| Konishi, Y. |
RELATION BETWEEN TRAILING EDGE NOISE AND BOUNDARY LAYER INSTABILITY |
ICAS2008-P2.14 |
| Konrath, R. |
DEVELOPMENT & APPLICATION OF MODERN MEASUREMENT TECHNIQUES FOR PRESSURIZED CRYOGENIC WIND TUNNELS |
ICAS 2008-3.2.1 |
| Konstanzer, P. |
PIEZO ACTIVE VIBRATION AND NOISE CONTROL IN HELICOPTERS |
ICAS 2008-4.9.2 INVITED |
| Kontis, K. |
THE INVESTIGATION OF DEPENDENCE OF LOW FREQUENCY MOTION ON UPSTREAM FLOW CONDITIONS IN HYPERSONIC FLOWS |
ICAS2008-3.7 ST: |
| Kopardekar, P. |
RELATIONSHIP OF MAXIMUM MANAGEABLE AIR TRAFFIC CONTROL COMPLEXITY AND SECTOR CAPACITY |
ICAS 2008-8.2.3 |
| Korn, B. |
PERFORMANCE-BASED TMA HANDLING FOR MIXED TRAFFIC USING A GROUND BASED 4D-GUIDANCE FOR UNEQUIPPED AIRCRAFT |
ICAS 2008-10.8.3 |
| Kos, J. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
| Kotegawa, T. |
UTILIZATION OF NETWORK THEORY FOR THE ENHANCEMENT OF ATO AIR ROUTE FORECAST |
ICAS 2008-11.10.5 (AIAA 2008-8944) |
| Kowalczyk, G. |
FLIGHT SAFETY AS CONSIDERED IN PROBABILISTIC TERMS |
ICAS 2008-9.3.4 |
| Kowalczyk, G. |
MODELING AND SIMULATION OF FLAPPING WINGS MICRO-AERIAL VEHICLES FLIGHT DYNAMICS |
ICAS 2008-5.9.1 INVITED |
| Kroo, I. M. |
MULTI-OBJECTIVE AIRCRAFT OPTIMIZATION FOR MINIMUM COST AND EMISSIONS OVER SPECIFIC ROUTE NETWORKS |
ICAS 2008-10.6.3 (AIAA 2008-8905) |
| Kroo, I. M. |
THEORETICAL AND EXPERIMENTAL INVESTIGATION OF ENERGY EXTRACTION FROM ATMOSPHERIC TURBULENCE |
ICAS2008-1.5 ST: |
| Krozel, J. |
CAUSALITY ANALYSIS FOR AVIATION WEATHER HAZARDS |
ICAS 2008-10.7.1 (AIAA 2008-8914) |
| Krozel, J. |
ON-DEMAND SPECIAL USE AIRSPACE |
ICAS 2008-10.10.4 (AIAA 2008-8938) |
| Krozel, J. |
TASK ANALYSIS FOR FEASIBILITY ASSESSMENT OF A COLLABORATIVE TRAFFIC FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.7.3 (AIAA 2008-8909) |
| Krüger, J. |
FLIGHT SIMULATORS – ON DIFFERENT PERCEPTIONS OF MANUFACTURERS, AVIATION AUTHORITIES, RESEARCH AND USERS |
ICAS 2008-5.5.1 INVITED |
| Krus, P. |
A QUANTIFIED RELATIONSHIP MATRIX AIDED BY PROBABILISTIC DESIGN AND OPTIMIZATION |
ICAS 2008-6.2.1 |
| Krus, P. |
AIRCRAFT CONCEPTUAL DESIGN AUTOMATION |
ICAS 2008-1.8.1 |
| Krus, P. |
COMPUTATIONAL TOOLS FOR AIRCRAFT SYSTEM ANALYSIS AND OPTIMIZATION |
ICAS 2008-1.8.2 |
| Krus, P. |
HOSTED SIMULATION FOR HETEROGENEOUS AIRCRAFT SYSTEM DEVELOPMENT |
ICAS2008-6.2 ST: |
| Kubinyi, M. |
EMAT APPLIED IN THE AVIATION INDUSTRY |
ICAS2008-P1.1 (AIAA 2008-8870) |
| Kubo, D. |
AUTONOMOUS AERIAL OBSERVATION SYSTEM FOR DISASTER RESPONSE USING ELECTRIC DUCTED FAN MAVS |
ICAS 2008-1.4.5 |
| Kubo, D. |
ROBUST OPTIMAL DESIGN OF AN AUTOPILOT FOR TRANSITIONAL FLIGHTS OF A TAIL-SITTER MINI UAV |
ICAS 2008-5.9.2 |
| Kuenz, A. |
PERFORMANCE-BASED TMA HANDLING FOR MIXED TRAFFIC USING A GROUND BASED 4D-GUIDANCE FOR UNEQUIPPED AIRCRAFT |
ICAS 2008-10.8.3 |
| Kuhlmann, A. |
IMPACT OF ESTOL CAPABILITY ON RUNWAY CAPACITY - AN ANALYTICAL APPROACH |
ICAS 2008-11.9.4 (AIAA 2008-8933) |
| Kulemin, A. V. |
ESTIMATION OF CRACK TURN PHENOMENON |
ICAS 2008-7.6.3 |
| Kulkarni, D. |
PREDICTION OF WEATHER-RELATED DELAYS IN THE CONTINENTAL UNITED STATES |
ICAS 2008-8.2.2 |
| Kumano, T. |
LOW-BOOM AND LOW-DRAG OPTIMIZATION FOR THE TWIN-ENGINE SILENT SUPERSONIC TECHNOLOGY DEMONSTRATOR |
ICAS 2008-2.4.1 |
| Kunin, A. |
PULSATING COMBUSTION OF AN ORGANIC GEL-FUEL DROPLET AND ITS INFLUENCE ON THE THERMAL FIELD OF A SPRAY DIFFUSION FLAME |
ICAS 2008-4.1.2 |
| Kupfer, M. |
AUTOMATED CONFLICT RESOLUTION - A SIMULATION-BASED SENSITIVITY STUDY OF AIRSPACE AND DEMAND |
ICAS 2008-8.9.1 |
| Kuratani, N. |
EXPERIMENTAL STUDY ON INTERFERENCE FLOW OF A SUPERSONIC BUSEMANN BIPLANE USING PRESSURE-SENSITIVE PAINT TECHNIQUE |
ICAS 2008-3.7.5 |
| Kuratani, N. |
WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION |
ICAS2008-2.4 ST: |
| Kuroda, F. |
NUMERICAL STUDY OF A PITOT PROBE WITH FIVE-HOLE PYRAMIDAL HEAD FOR SUPERSONIC FLIGHT TEST |
ICAS 2008-3.2.4 |
| Kurotaki, T. |
HIGH-ORDER LARGE EDDY SIMULATION AROUND 2-D AEROFOIL WITH HIGH-LIFT DEVICE |
ICAS 2008-2.1.2 |
| Kurotaki, T. |
INTERFACE CONDITIONS OF FINITE-DIFFERENCE COMPACT SCHEMES FOR COMPUTATIONAL AEROACOUSTICS |
ICAS 2008-2.3.1 |
| Kurotaki, T. |
LARGE EDDY SIMULATION AROUND 2-D AIRFOIL WITH NATURAL TRANSITION AT HIGH REYNOLDS NUMBERS |
ICAS2008-2.1 ST: |
| Kuzminski, P. |
AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
| Kwak, D. Y. |
FLIGHT TEST RESULTS AT TRANSONIC REGION ON SUPERSONIC EXPERIMENTAL AIRPLANE (NEXST-1) |
ICAS 2008-2.4.2 |
| Kwak, D. Y. |
NUMERICAL STUDY OF A PITOT PROBE WITH FIVE-HOLE PYRAMIDAL HEAD FOR SUPERSONIC FLIGHT TEST |
ICAS 2008-3.2.4 |
| Kwak, D. Y. |
VORTEX BEHAVIORS OF CRANKED ARROW WING CONFIGURATIONS WITH DIFFERENT WING PLANFORMS |
ICAS 2008-3.3.2 |
| Kwan, J. S. |
MODEL-BASED AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.1 (AIAA 2008-8907) |
| La Rocca, G. |
CONTROLLABILITY OF BLENDED WING BODY AIRCRAFT |
ICAS 2008-5.4.3 |
| La Rocca, G. |
KNOWLEDGE BASED ENGINEERING TO SUPPORT AIRCRAFT MULTIDISCIPLINARY DESIGN AND OPTIMISATION |
ICAS 2008-6.10.1 |
| Laban, M. |
OPTIMISING HIGH-EFFICIENCY RUDDERS FOR TRANSPORT AIRCRAFT FUEL BURN REDUCTION |
ICAS 2008-2.11.2 |
| Lagu, A. V. |
A SYSTEM SAFETY FRAMEWORK FOR ANALYZING FUTURE AIR TRANSPORTATION SEPARATION ASSURANCE AND COLLISION AVOIDANCE CONCEPTS |
ICAS 2008-11.4.3 (AIAA 2008-8883) |
| Lai, J. C. S. |
FLAPPING-WING TECHNOLOGY: THE POTENTIAL FOR AIR VEHICLE PROPULSION AND AIRBORNE POWER GENERATION |
ICAS 2008-1.5.1 |
| Landry, S. J. |
A SYSTEM SAFETY FRAMEWORK FOR ANALYZING FUTURE AIR TRANSPORTATION SEPARATION ASSURANCE AND COLLISION AVOIDANCE CONCEPTS |
ICAS 2008-11.4.3 (AIAA 2008-8883) |
| Langhans, S. |
A HOLISTIC APPROACH TO EVALUATE THE AIR TRANSPORTATION SYSTEM |
ICAS 2008-8.4.2 |
| Lanier, R. C. |
TAILORED ARRIVALS OPERATIONS AT SFO AND EXPECTED ENVIRONMENTAL BENEFITS |
ICAS 2008-11.3.4 (AIAA 2008-8868) |
| Larocca, F. |
EULER INVERSE THROUGHFLOW MODEL BASED ON AN IMPLICIT UPWIND TIME MARCHING TECHNIQUE |
ICAS 2008-2.3.2 |
| Laroche, P. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
| Laschka, B. |
SMALL DISTURBANCE NAVIER-STOKES COMPUTATIONS FOR LOW ASPECT RATIO WING PITCHING OSCILLATIONS |
ICAS 2008-2.10.3 |
| Lauderdale, T. A. |
PREDICTIVE MODELS OF THE NATIONAL AIRSPACE SYSTEM USING BAYESIAN NETWORKS |
ICAS 2008-8.4.4 |
| Lavelle, T. |
COUPLED HIGH-FIDELITY ENGINE SYSTEM SIMULATION |
ICAS 2008-8.10.3 INVITED |
| Lawson, C. P. |
DESIGN AND DEVELOPMENT OF THE ECLIPSE AND DEMON DEMONSTRATOR UAVS |
ICAS 2008-1.4.2 |
| Lawson, C. P. |
THE STATE-OF-THE-ART AND THE FUTURE OF WATER MANAGEMENT WITHIN FUEL TANKS |
ICAS2008-6.4 ST: |
| Lawson, C. P. |
THERMAL MANAGEMENT OF ELECTROMECHANICAL ACTUATION ON AN ALL-ELECTRIC AIRCRAFT |
ICAS 2008-6.6.2 |
| Le Tallec, C. |
INNOVATIVE FUTURE AIR TRANSPORT SYSTEM: SIMULATION OF A FULLY AUTOMATED ATS |
ICAS 2008-8.4.5 |
| Lee, B. |
THEORETICAL APPROACH TO DIRECTIONAL CONTROL SENSITIVITY SELECTION |
ICAS 2008-5.4.1 INVITED |
| Lee, D. |
AVIATION CLIMATE IMPACT - A SUMMARY OF ONGOING EUROPEAN RESEARCH PROGRAMMES |
ICAS 2008-0.3 |
| Lee, D. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
| Lee, J. |
SIMULATION OF A NON-AXISYMMETRIC UNDERSEA VEHICLE USING A RECURSIVE NEURAL NETWORK |
ICAS 2008-5.8.2 |
| Lee, J. H. |
DESIGN AND OPERATION OF THE ADD ENVIRONMENTAL TEST FACILITY |
ICAS2008-P6.6 |
| Lee, J. -W. |
A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
| Lee, K. |
CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
| Lee, P. U. |
CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
| Lee, S. |
UNSTEADY AERODYNAMIC ANALYSIS OF HELICOPTER ROTOR BY USING THE TIME-DOMAIN PANEL METHOD |
ICAS2008-2.10 ST: |
| Lefebvre, T. |
AERODYNAMIC AND AERO-ACOUSTIC DESIGN OF MODERN TILT-ROTORS: THE ONERA EXPERIENCE |
ICAS 2008-1.7.4 |
| Legge, J. |
DEPARTURE TAXI TIME PREDICTIONS USING ASDE-X SURVEILLANCE DATA |
ICAS 2008-11.11.1 (AIAA 2008-8958) |
| Lehmann, O. |
RESEARCH ON INTEGRATED COLLIMATED COCKPIT VISUAL AND FLIGHT INFORMATION SYSTEM |
ICAS 2008-9.10.1 |
| Lehner, S. |
COMBINATORIAL OPTIMIZATION TO INCLUDE GREENER TECHNOLOGIES IN A SHORT-TO-MEDIUM RANGE COMMERCIAL AIRCRAFT |
ICAS 2008-4.10.2 (AIAA 2008-8963) |
| Lei, Z. |
WING DESIGN OF SUPERSONIC TRANSPORT BY A MULTI-POINT OPTIMIZATION METHOD |
ICAS 2008-2.4.3 |
| Leijonhufvud, M. C. |
DYNAMIC SIMULATION OF A TOWED DECOY SYSTEM |
ICAS 2008-5.11.1 |
| Lemmen, H. J. K. |
THE INFLUENCE OF FATIGUE CRACK INITIATION BEHAVIOUR OF FRICTION STIR WELDED JOINTS ON THE DESIGN CRITERIA |
ICAS 2008-7.6.2 |
| Lemmers, A. J. J. |
THREAT ASSESSMENT AND RESPONSE MANAGEMENT SYSTEM TARMS: AN ON-BOARD AIRCRAFT SECURITY SYSTEM |
ICAS 2008-9.1.2 |
| Lemoine, M. |
THE IMPACT OF RIGOROUS METHODS ON AERONAUTICAL REGULATIONS |
ICAS 2008-9.7.1 |
| Lempia, D. |
USING LEAN PRINCIPLES AND MBE IN DESIGN AND DEVELOPMENT OF AVIONICS EQUIPMENT AT ROCKWELL COLLINS |
ICAS 2008-6.7.3 |
| Lenz, H. |
AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION FOR TAKE-OFF AND DEPARTURE |
ICAS 2008-11.8.3 (AIAA 2008-8921) |
| Lenz, H. |
GENERATION OF HIGH ACCURATE 4D TRAJECTORIES FOR TAKE-OFF AND DEPARTURE |
ICAS2008-8.11 ST: |
| Lenz, J. |
UNIQUE PERFORMANCE CHARACTERISTICS OF SOLAR AIRCRAFT |
ICAS 2008-5.3.2 |
| Leuckert, J. |
DEVELOPMENT & APPLICATION OF MODERN MEASUREMENT TECHNIQUES FOR PRESSURIZED CRYOGENIC WIND TUNNELS |
ICAS 2008-3.2.1 |
| Levin, K. |
INTEGRATED TIME-BASED FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.10.1 (AIAA 2008-8940) |
| Levy, B. |
DEPARTURE TAXI TIME PREDICTIONS USING ASDE-X SURVEILLANCE DATA |
ICAS 2008-11.11.1 (AIAA 2008-8958) |
| Lewe, J. -H. |
ADVANCED GENERAL AVIATION DESIGN WITH TRANSPORTATION ARCHITECTURE ANALYSIS |
ICAS 2008-1.9.4 (AIAA 2008-8929) |
| Lewe, J. -H. |
DEMAND-CENTRIC ANALYSIS OF THE AIR TRANSPORTATION SYSTEM |
ICAS 2008-10.4.3 (AIAA 2008-8889) |
| Lewitowicz, J. |
MODELING AND SIMULATION OF FLAPPING WINGS MICRO-AERIAL VEHICLES FLIGHT DYNAMICS |
ICAS 2008-5.9.1 INVITED |
| Lewitowicz, J. L. |
FLIGHT SAFETY AS CONSIDERED IN PROBABILISTIC TERMS |
ICAS 2008-9.3.4 |
| Lhommeau, T. |
RELIABILITY STUDY OF POWER MODULE BY STOCHASTIC UNCERTAINTY METHOD FOR AN AERONAUTICAL APPLICATION |
ICAS 2008-6.1.1 |
| Li, A. |
REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
| Li, B. F. |
COORDINATELY MODELING AND SIMULATION OF THE EJECTION SEAT/OCCUPANT SYSTEM |
ICAS2008-P9.3 |
| Li, D. |
AN APPROXIMATION METHOD FOR THE NUMERICAL SIMULATION ON UNSTEADY FLOWS AROUND SMALL-DISPLACEMENT MOVING OBJECTS |
ICAS2008-3.9 ST: |
| Li, D. |
LIFT PREDICTION OF MULTI-ELEMENT AIRFOIL USING DES AND RANS |
ICAS2008-P2.5 |
| Li, G. |
TEST DATA MANAGEMENT FOR AIRCRAFT HYDRAULIC SYSTEM TESTING |
ICAS2008-P6.3 |
| Li, H. C. H. |
LOADED CARBON COMPOSITE SCARF JOINTS SUBJECT TO QUASI STEADY LATERAL LOADS |
ICAS 2008-7.2.2 |
| Li, J. S. |
NEW METHOD TO ENHANCE THE WEARABILITY OF TITANIUM ALLOY ROTOR BLADE FOR AERO-ENGINE |
ICAS 2008-4.2.4 |
| Li, M. |
MISSION DECISION-MAKING METHOD OF MULTI-AIRCRAFT COOPERATIVELY ATTACKING MULTI-TARGET BASED ON SITUATIONAL ASSESSMENT |
ICAS2008-P1.2 |
| Li, M. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
| Li, M. |
SECURITY OF WIRELESS SENSOR NETWORK ENABLED HEALTH MONITORING FOR FUTURE AIRPLANES |
ICAS 2008-9.1.3 |
| Li, W. |
MULTIDISCIPLINARY DESIGN, ANALYSIS, AND OPTIMIZATION TOOL DEVELOPMENT USING GENETIC ALGORITHM |
ICAS 2008-1.1.1 |
| Li, W. J. |
A NEW EFFICIENT INTERACTIVE MULTI-OBJECTIVE EVOLUTIONARY OPTIMIZATION ALGORITHM AND APPLICATION IN ENGINEERING |
ICAS2008-6.2 ST: |
| Li, Y. |
AN APPROACH FOR MULTI-CRITERIA DECISION MAKING METHOD SELECTION AND DEVELOPMENT |
ICAS 2008-1.3.1 |
| Li, Z. |
EXTENDING FMC TEST FOR FLIGHT SIMULATION AND FLIGHT EXPERIMENTS |
ICAS 2008-5.5.3 |
| Li, Z. S. |
DEVELOPMENT OF FLIGHT CONTROL SYSTEM USING EMBEDDED COMPUTER PC-104 |
ICAS2008-P5.1 |
| Liang, X. G. |
CFD RESEARCH FOR AIR-TO-AIR MISSILE WITH LATERAL JET CONTROL |
ICAS2008-2.64 ST: |
| Liang, Y. M. |
NEW METHOD TO ENHANCE THE WEARABILITY OF TITANIUM ALLOY ROTOR BLADE FOR AERO-ENGINE |
ICAS 2008-4.2.4 |
| Liao, M. |
STATIC AND FATIGUE ANALYSIS OF AN UPPER WING SKIN WITH EXFOLIATION CORROSION |
ICAS 2008-7.4.1 |
| Lijewski, L. |
IHAAA STORE SEPARATION FROM CAVITY (SSC) PROJECT |
ICAS 2008-2.6.2 |
| Lim, K. M. |
THE STATE-OF-THE-ART AND THE FUTURE OF WATER MANAGEMENT WITHIN FUEL TANKS |
ICAS2008-6.4 ST: |
| Lin, G. P. |
A LAYER PAVEMENT MODEL TO SIMULATE ROUGHNESS FEATURES IN ICE ACCRETION NUMERICAL SIMULATION |
ICAS 2008-2.6.1 |
| Lin, K. Y. |
PROBABILISTIC MODELING OF STRUCTURAL / AEROELASTIC LIFE CYCLE FOR RELIABILITY EVALUATION OF DAMAGE TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.1.1 |
| Lind, I. |
HOSTED SIMULATION FOR HETEROGENEOUS AIRCRAFT SYSTEM DEVELOPMENT |
ICAS2008-6.2 ST: |
| Lindberg, A. |
DYNAMIC SIMULATION OF A TOWED DECOY SYSTEM |
ICAS 2008-5.11.1 |
| Lindberg, A. |
TRANSONIC STORE SEPARATION STUDIES ON THE SAAB GRIPEN AIRCRAFT USING COMPUTATIONAL AERODYNAMICS |
ICAS 2008-2.9.1 |
| Lindeblad, M. |
VIRTUAL ENTERPRISE COLLABORATION - BREAKTHROUGH TECHNOLOGIES PROVIDED BY VIVACE |
ICAS 2008-8.10.4 INVITED |
| Lindell, H. |
GRIPEN, PROGRAM OVERVIEW AND FUTURE DEVELOPMENT |
ICAS 2008-1.7.5 |
| Lindholm, T. |
CAUSALITY ANALYSIS FOR AVIATION WEATHER HAZARDS |
ICAS 2008-10.7.1 (AIAA 2008-8914) |
| Lintelman, S. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
| Liscouet, J. |
AUTOMATED GENERATION, SELECTION AND EVALUATION OF ARCHITECTURES FOR ELECTROMECHANICAL ACTUATORS |
ICAS 2008-6.6.1 |
| Liscouët-Hanke, S. |
A SIMULATION FRAMEWORK FOR AIRCRAFT POWER SYSTEMS ARCHITECTING |
ICAS 2008-6.2.4 |
| Littman, D. |
TOWARD AN ECONOMIC MODEL TO INCENTIVIZE VOLUNTARY OPTIMIZATION OF NAS TRAFFIC FLOW |
ICAS 2008-10.4.1 (AIAA 2008-8887) |
| Liu, F. |
NUMERICAL RESEARCHES ON THE AEROELASTIC PROBLEM OF TURBOMACHINERY |
ICAS 2008-4.4.4 |
| Liu, H. |
AN UPDATING PROGRAM FOR UNDERGRADUATE AIRCRAFT CONCEPTUAL AND PRELIMINARY DESIGN COURSE |
ICAS2008-P1.5 |
| Liu, J. |
FATIGUE BEHAVIOR AND LIFE PREDICTION OF WELDED TITANIUM ALLOY JOINTS |
ICAS 2008-7.4.4 |
| Liu, W. T. |
3 A STUDY ON FATIGUE SCATTER FACTOR OF INDIVIDUAL AIRCRAFT STRUCTURE |
ICAS2008-P3.1 |
| Liu, Y. |
RESEARCH ON CONTROL ALLOCATION FOR AIRCRAFTS WITH MULTIPLE CONTROL EFFECTORS |
ICAS 2008-5.2.4 |
| Liu, Y. |
RESEARCH ON FUZZY LOGIC PIO DETECTOR |
ICAS 2008-5.4.5 |
| Liu, Z. |
AERODYNAMICS CHARACTERISTICS OF HYPERSONIC VEHICLE IN NEAR SPACE |
ICAS2008-2.5 ST: |
| Liu, Z. |
ANALYSIS OF THE SCATTERING CHARACTERISTICS FROM DISCONTINUITY SURFACES ON AIRCRAFT USING A MODIFIED MLFMA |
ICAS2008-P3.6 |
| Livne, E. |
PROBABILISTIC MODELING OF STRUCTURAL / AEROELASTIC LIFE CYCLE FOR RELIABILITY EVALUATION OF DAMAGE TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.1.1 |
| Lock, G. |
AN EXPERIMENTAL AND COMPUTATIONAL STUDY OF LOW RE NUMBER TRANSITIONAL FLOWS OVER AN AEROFOIL WITH LEADING EDGE SLAT |
ICAS2008-P2.1 (AIAA 2008-8877) |
| Lohr, G. |
INFORMATION REQUIREMENTS FOR SUPERVISORY AIR TRAFFIC CONTROLLERS IN SUPPORT OF A MID-TERM WAKE VORTEX DEPARTURE SYSTEM |
ICAS 2008-8.11.3 |
| Lohr, G. |
WAKE TURBULENCE MITIGATION FOR ARRIVALS (WTMA) |
ICAS 2008-9.9.3 |
| Lombaerts, T. J. J. |
A SIMULATION BENCHMARK FOR AIRCRAFT SURVIVABILITY ASSESSMENT |
ICAS 2008-9.3.2 |
| Lopez Ruiz, E. R. |
THE IMPACT OF RIGOROUS METHODS ON AERONAUTICAL REGULATIONS |
ICAS 2008-9.7.1 |
| Lourencao, P. T. M. |
EVOLUTION OF EMBRAER’S CIVIL AIRCRAFT |
ICAS 2008-1.7.1 INVITED |
| Lozito, S. |
FLIGHT DECK PROCEDURAL GUIDELINES FOR DATALINK TRAJECTORY NEGOTIATIONS |
ICAS 2008-11.6.4 (AIAA 2008-8901) |
| Lozito, S. |
PRELIMINARY GUIDELINES ON FLIGHT DECK PROCEDURES FOR VERY CLOSELY SPACED PARALLEL APPROACHES |
ICAS 2008-8.5.2 |
| Lu, G. Z. |
INTEGRATED PREDICTION OF MACROSCOPIC PROPERTIES OF COMPOSITES BASED ON FINITE ELEMENT COMPUTATIONAL MICROMECHANICS |
ICAS2008-7.9 ST: |
| Lu, S. L. |
INTEGRATED PREDICTION OF MACROSCOPIC PROPERTIES OF COMPOSITES BASED ON FINITE ELEMENT COMPUTATIONAL MICROMECHANICS |
ICAS2008-7.9 ST: |
| Lu, Y. |
INTEGRATED PREDICTION OF MACROSCOPIC PROPERTIES OF COMPOSITES BASED ON FINITE ELEMENT COMPUTATIONAL MICROMECHANICS |
ICAS2008-7.9 ST: |
| Luan, Y. C. |
THE SIMULATION OF THE HUMAN-MACHINE PARTNERSHIP IN UCAV OPERATION |
ICAS 2008-9.10.5 |
| Luber, G. |
APPLICATION OF PVDF FOILS FOR THE MEASUREMENTS OF UNSTEADY PRESSURES ON WIND TUNNEL MODELS FOR THE PREDICTION OF AIRCRAFT VIBRATIONS |
ICAS 2008-3.4.2 |
| Luckner, R. |
PILOTED SIMULATION RESULTS OF AN ONBOARD WAKE VORTEX DETECTION, WARNING AND AVOIDANCE SYSTEM AND COCKPIT DISPLAY ASPECTS |
ICAS 2008-9.9.1 |
| Ludwig, T. |
UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
| Luks, N. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
| Lundström, D. |
RAVEN – A SUBSCALE RADIO CONTROLLED BUSINESS JET DEMONSTRATOR |
ICAS 2008-5.5.2 |
| Lung, S. -F. |
STRUCTURAL MODEL TUNING CAPABILITY IN AN OBJECT-ORIENTED MULTIDISCIPLINARY DESIGN, ANALYSIS, AND OPTIMIZATION TOOL |
ICAS 2008-9.5.1 |
| Lunnon, B. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
| Lunsford, C. R. |
SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
| Luxhoj, J. T. |
HAZARD, SAFETY RISK AND UNCERTAINTY MODELING OF THE INTEGRATION OF UNMANNED AIRCRAFT SYSTEMS INTO THE NATIONAL AIRSPACE |
ICAS 2008-9.7.2 |
| Lv, M. |
THE APPLICATION OF AIRBORNE VIDEO TECHNOLOGIES DURING AERIAL REFUELING TEST |
ICAS2008-P5.2 |
| Lyrsell, O. |
A STUDY OF AN USER AND ENVIRONMENTAL FRIENDLY STORED ENERGY BASED EPU/APU-SYSTEM FOR MILITARY AEROSPACE APPLICATIONS |
ICAS 2008-6.4.5 |
| Maciel, E. S. de Góes |
SOLUTIONS OF INVISCID AND VISCOUS FLOWS USING STRUCTURED HIGH RESOLUTION ALGORITHMS IN THREE-DIMENSIONS |
ICAS2008-P2.7 |
| Macke, O. |
DESIGN OF 4D LANDING APPROACH TRAJECTORIES FOR A QUIET STOL AIRPLANE |
ICAS 2008-4.8.2 |
| Macke, O. |
EVALUATION OF SIMULATOR AND FLIGHT TESTED NOISE ABATEMENT APPROACH PROCEDURES |
ICAS 2008-4.8.1 |
| MacWilliams, P. V. |
TERMINAL AREA REQUIRED TIME OF ARRIVAL (RTA) CONCEPT OF OPERATIONS AND AUTOMATION PROTOTYPE |
ICAS 2008-11.9.1 (AIAA 2008-8930) |
| Maeng, J. S. |
UNSTEADY PROPULSIVE CHARACTERISTICS OF BIOFOILS MOVING IN A VERY LOW-REYNOLDS NUMBER FLOW |
ICAS 2008-3.9.3 |
| Magyarits, S. |
RELATIONSHIP OF MAXIMUM MANAGEABLE AIR TRAFFIC CONTROL COMPLEXITY AND SECTOR CAPACITY |
ICAS 2008-8.2.3 |
| Maidl, M. |
SECURITY ARCHITECTURE AND FORMAL ANALYSIS OF AN AIRPLANE SOFTWARE DISTRIBUTION SYSTEM |
ICAS 2008-9.1.1 |
| Maier, R. |
MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
| Maier, R. |
PIEZO ACTIVE VIBRATION AND NOISE CONTROL IN HELICOPTERS |
ICAS 2008-4.9.2 INVITED |
| Maisto, U. |
SINGLE VERSUS MULTIPLE WINGLETS: NUMERICAL AND EXPERIMENTAL INVESTIGATION |
ICAS 2008-2.7.3 |
| Makida, M. |
DEVELOPMENT OF FULL ANNULAR COMBUSTOR FOR SMALL AIRCRAFT JET ENGINE IN JAXA TECHCLEAN PROJECT |
ICAS 2008-4.3.2 |
| Malbéqui, P. |
A NOVEL APPROACH TO AIR TRANSPORT SYSTEM ENVIRONMENTAL IMPACT EVALUATION THROUGH PHYSICAL MODELLING AND SIMULATION |
ICAS2008-8.3 ST: |
| Malis, M. |
INNOVATIVE COMPOSITE STRUCTURES FOR SMALL AIRCRAFT |
ICAS2008-7.3 ST: |
| Malone-Lee, J. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
| Malwitz, A. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
| Mamou, M. |
COMPUTATIONAL FLUID DYNAMICS AND EXPERIMENTAL INVESTIGATION OF AIRPLANE STALL DYNAMICS WITH WING CONTAMINATION |
ICAS 2008-3.5.2 |
| Mandanis, G. |
UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
| Mane, M. |
BASE OF OPERATIONS CONCEPT FOR ON-DEMAND OPERATIONS |
ICAS 2008-8.6.4 (AIAA 2008-8977 ) |
| Mane, M. |
CONCURRENT AIRCRAFT DESIGN AND RESOURCE ALLOCATION UNDER UNCERTAINTY FOR ON-DEMAND AIR TRANSPORTATION |
ICAS 2008-10.6.1 (AIAA 2008-8903) |
| Mani, M. |
A HYBRID, DYNAMIC LARGE EDDY SIMULATION METHOD |
ICAS 2008-2.1.1 |
| Manipurath, S. |
DEVELOPMENT OF AN INDUSTRIAL SCALE COMBUSTION TEST AND RESEARCH FACILITY FOR ALTERNATIVE FUELS AND FUEL FLEXIBILITY DEMONSTRATION |
ICAS 2008-4.3.1 |
| Mansouri, G. |
HEALTH MONITORING FOR COMMERCIAL AIRCRAFT SYSTEMS |
ICAS 2008-6.1.2 |
| Mantegazza, P. |
DEVELOPMENT AND VALIDATION OF AN INVESTIGATION TOOL FOR NONLINEAR AEROELASTIC ANALYSIS |
ICAS 2008-9.6.3 |
| Mantilla, J. G. |
PAYLOAD FUEL ENERGY EFFICIENCY AS A METRIC FOR AVIATION ENVIRONMENTAL PERFORMANCE |
ICAS 2008-4.7.4 |
| Manzato, D. |
A NEW AIRCRAFT CONCEPT: THE COMBAT MALE |
ICAS 2008-1.4.4 |
| Marcotte, D. |
FLIGHT EVALUATION OF A COMPACT AIRBORNE TRACE GAS ANALYSIS SENSOR PROOF-OF-CONCEPT |
ICAS2008-P6.4 |
| Maré, J.-C. |
AUTOMATED GENERATION, SELECTION AND EVALUATION OF ARCHITECTURES FOR ELECTROMECHANICAL ACTUATORS |
ICAS 2008-6.6.1 |
| Marinkovski, D. |
APPLICATION OF SEMICONDUCTOR STRAIN GAUGES IN MEASUREMENTS OF DYNAMIC STABILITY DERIVATIVES IN THE T-38 WIND TUNNEL |
ICAS 2008-3.4.5 |
| Marissen, R. |
CARBON/DYNEEMA INTRALAMINAR HYBRIDS: NEW STRATEGY TO INCREASE IMPACT RESISTANCE OR DECREASE MASS OF CARBON FIBER COMPOSITES |
ICAS 2008-7.3.4 |
| Markovic, D. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
| Maroney, D. |
NEXTGEN AND SESAR: OPPORTUNITIES FOR UAS INTEGRATION |
ICAS 2008-10.8.2 (AIAA 2008-8925) |
| Marques, F. D. |
AERO-STRUCTURAL MDO OF A SPAR-TANK-TYPE WING FOR AIRCRAFT CONCEPTUAL DESIGN |
ICAS2008-1.1 ST: |
| Marques, F. D. |
DYNAMIC ANALYSIS OF AEROELASTIC RESPONSE FOR TRANSONIC FLOW WITH NONLINEAR STRUCTURAL MODEL |
ICAS 2008-9.6.4 |
| Marques, J. M. G. |
ON THE MINIMIZATION OF CRUISE DRAG DUE TO PITCH TRIM FOR A FLYING-WING CONFIGURATION |
ICAS 2008-5.3.3 |
| Marques, J. M. G. |
ON THE PROBABILITY OF COLLISION FOR CLIMBING AND DESCENDING TRAJECTORIES RELEVANT TO AIR TRAFFIC MANAGEMENT |
ICAS2008-9.3 ST: |
| Marsden, A. |
OPERATIONAL CONCEPT FOR AN AIRPORT OPERATIONS CENTER TO ENABLE TOTAL AIRPORT MANAGEMENT |
ICAS 2008-8.3.2 |
| Martin, C. |
RELIABILITY STUDY OF POWER MODULE BY STOCHASTIC UNCERTAINTY METHOD FOR AN AERONAUTICAL APPLICATION |
ICAS 2008-6.1.1 |
| Martinez-Val, R. |
AIRPLANE DESIGN: A MUST IN AERONAUTICAL ENGINEERING EDUCATION |
ICAS2008-P1.6 |
| Martinez-Val, R. |
FLIGHT DYNAMICS OF THE FLYING WING |
ICAS 2008-5.8.3 |
| Martins, A. L. |
A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
| Marulo, F. |
FE STUDY OF WINDSHIELD SUBJECTED TO HIGH SPEED BIRD IMPACT |
ICAS 2008-9.4.3 |
| Marulo, F. |
PRACTICAL AEROELASTIC CALCULATIONS FOR LIGHT AIRPLANES |
ICAS2008-7.7 ST: |
| Maruyama, D. |
AERODYNAMIC DESIGN OF THREE-DIMENSIONAL BIPLANE WINGS FOR LOW-WAVE DRAG SUPERSONIC FLIGHT |
ICAS 2008-2.4.4 |
| Masahiro, K. |
COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA |
ICAS 2008-2.2.1 |
| Masarati, P. |
BIOMECHANICAL PILOT PROPERTIES IDENTIFICATION BY INVERSE KINEMATICS/INVERSE DYNAMICS MULTIBODY ANALYSIS |
ICAS 2008-9.10.4 |
| Masarati, P. |
DEVELOPMENT AND VALIDATION OF AN INVESTIGATION TOOL FOR NONLINEAR AEROELASTIC ANALYSIS |
ICAS 2008-9.6.3 |
| Masui, K. |
RESEARCH AND DEVELOPMENT FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM - PART 2 FLIGHT EXPERIMENTS |
ICAS 2008-5.10.2 |
| Matejka, M. |
SEPARATION CONTROL BY SYNTHETIC JET ACTUATOR IN STRAIGHT BLADE CASCADE |
ICAS 2008-3.10.4 |
| Matsuno, T. |
FOREBODY VORTEX CONTROL ON HIGH PERFORMANCE AIRCRAFT USING PWM-CONTROLLED PLASMA ACTUATORS |
ICAS 2008-3.3.4 |
| Mattaboni, M. |
BIOMECHANICAL PILOT PROPERTIES IDENTIFICATION BY INVERSE KINEMATICS/INVERSE DYNAMICS MULTIBODY ANALYSIS |
ICAS 2008-9.10.4 |
| Mattiazzo, G. |
FLY-BY-WIRE CONTROL OF A HELICOPTER: MULTIBODY MAIN ROTOR MODEL |
ICAS2008-5.11 ST: |
| Mattos, W. S. |
APPLICATION OF A MODEL UPDATING METHOD TO AN AIRCRAFT LONGITUDINAL STABILITY AUGMENTATION SYSTEM |
ICAS2008-5.2 ST: |
| Maurice, L. |
GOING GREEN – MITIGATING AVIATION’S NEW ENVIRONMENTAL DRIVERS |
ICAS 2008-4.7.2 |
| Maurice, L. |
THE FEASIBILITY AND POTENTIAL ENVIRONMENTAL BENEFITS OF ALTERNATIVE FUELS FOR COMMERCIAL AVIATION |
ICAS 2008-4.7.5 |
| Mavris, D. |
A METHODOLOGICAL APPROACH FOR AIRPORT TECHNOLOGY EVALUATION AND SELECTION |
ICAS 2008-8.3.4 (AIAA 2008-8965) |
| Mavris, D. |
AN APPROACH FOR MULTI-CRITERIA DECISION MAKING METHOD SELECTION AND DEVELOPMENT |
ICAS 2008-1.3.1 |
| Mavris, D. |
FUNCTION BASED ARCHITECTURE DESIGN SPACE DEFINITION AND EXPLORATION |
ICAS 2008-1.9.3 (AIAA 2008-8928) |
| Mavris, D. |
METHODOLOGY FOR AIRCRAFT SYSTEM ARCHITECTURE SIZING |
ICAS 2008-6.2.2 |
| Mavris, D. |
PARAMETRIC MODELING OF AN ELECTRICAL TEST RIG FOR POWER OPTIMIZED AIRCRAFT ARCHITECTURES |
ICAS2008-6.6 ST (AIAA 2008-8973) |
| Mavris, D. N. |
ADVANCED GENERAL AVIATION DESIGN WITH TRANSPORTATION ARCHITECTURE ANALYSIS |
ICAS 2008-1.9.4 (AIAA 2008-8929) |
| Mavris, D. N. |
AN APPROACH FOR VERIFICATION AND VALIDATION OF THE ENVIRONMENTAL DESIGN SPACE |
ICAS2008-P8.4 (AIAA 2008-8875) |
| Mavris, D. N. |
DEMAND-CENTRIC ANALYSIS OF THE AIR TRANSPORTATION SYSTEM |
ICAS 2008-10.4.3 (AIAA 2008-8889) |
| Mavris, D. N. |
PARAMETRIC SYSTEM EFFECTIVENESS ANALYSIS USING ARTIFICIAL NEURAL NETWORKS FOR BATTLE MANAGEMENT |
ICAS 2008-1.3.3 |
| Mavris, D. N. |
THE ENVIRONMENTAL DESIGN SPACE |
ICAS 2008-4.7.3 |
| Mayer, R. H. |
BENEFIT POTENTIAL OF CONTINUOUS CLIMB AND DESCENT OPERATIONS |
ICAS 2008-11.8.2 (AIAA 2008-8920) |
| Mayer, R. H. |
IMPROVING TERMINAL OPERATIONS - BENEFITS OF RNAV DEPARTURE PROCEDURES AT DALLAS-FORT WORTH AND HARTSFIELD-JACKSON ATLANTA INTERNATIONAL AIRPORTS |
ICAS 2008-11.1.3 (AIAA 2008-8856) |
| Mayo, J. |
AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
| Mazlum, E. |
A COMPARISON OF NUMERICAL RANS SIMULATIONS AND FLOW FIELD MEASUREMENTS OF AN OSCILLATING AIRFOIL FOR FLAPPING WING PROPULSION |
ICAS 2008-2.10.2 |
| Mazzotta, D. |
METHODOLOGY OPTIMIZATION OF METAL CUTTING PROGRAMMING APPLIED TO AERONAUTICAL COMPONENTS |
ICAS 2008-6.10.5 |
| McAlleenen, C. |
AEROSPACE PRODUCT COST MANAGEMENT AT THE EARLY CONCEPT OPERATIONS PHASE |
ICAS 2008-10.6.2 (AIAA 2008-8904) |
| McClean, A. |
USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
| McCoy, P. |
DESIGN FOR PROCESS EXCELLENCE - ENSURING TIMELY AND COST EFFECTIVE SOLUTIONS |
ICAS 2008-6.7.4 |
| McNally, D. |
AUTOMATED SEPARATION ASSURANCE IN THE PRESENCE OF UNCERTAINTY |
ICAS 2008-8.11.1 |
| McNichols, W. M. |
CAUSALITY ANALYSIS FOR AVIATION WEATHER HAZARDS |
ICAS 2008-10.7.1 (AIAA 2008-8914) |
| McRoberts, R. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
| Mead, R. |
TAILORED ARRIVALS OPERATIONS AT SFO AND EXPECTED ENVIRONMENTAL BENEFITS |
ICAS 2008-11.3.4 (AIAA 2008-8868) |
| Mébarki, Y. |
COMPUTATIONAL FLUID DYNAMICS AND EXPERIMENTAL INVESTIGATION OF AIRPLANE STALL DYNAMICS WITH WING CONTAMINATION |
ICAS 2008-3.5.2 |
| Mébarki, Y. |
TARGETING PODS EFFECTS ON STORE SEPARATION CHARACTERISTICS: A JOINT NRC-IAR/USNAVY CFD EFFORT |
ICAS 2008-2.9.2 |
| Meier, C. |
OPERATIONAL CONCEPT FOR AN AIRPORT OPERATIONS CENTER TO ENABLE TOTAL AIRPORT MANAGEMENT |
ICAS 2008-8.3.2 |
| Melby, P. |
BENEFIT POTENTIAL OF CONTINUOUS CLIMB AND DESCENT OPERATIONS |
ICAS 2008-11.8.2 (AIAA 2008-8920) |
| Melia, J. |
A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
| Mellert, V. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
| Mello Jr., A. W. S. |
SIMPLIFYING MSD MODELING BY USING CONTINUING DAMAGE ASSUMPTION AND PARAMETRIC STUDY: THE ROLE OF RIVET SQUEEZE FORCE |
ICAS 2008-9.8.1 |
| Mendez, J. |
FATIGUE DESIGN OF METALLIC COMPONENTS CONTAINING SURFACE OR INTERNAL DEFECTS |
ICAS 2008-7.4.3 |
| Mendez, J. |
SIZE OPTIMIZATION OF AIRCRAFT STRUCTURES |
ICAS2008-7.11 ST: |
| Menéndez, X. P. |
CAPACITY MODELLING FOR FUTURE AERONAUTICAL SAFETY COMMUNICATIONS OVER WIDE AREAS |
ICAS 2008-8.8.2 (AIAA 2008-8952) |
| Menon, P. K. |
MODEL-BASED AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.1 (AIAA 2008-8907) |
| Menon, P. K. |
QUEUEING NETWORK MODELS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.10.3 (AIAA 2008-8942) |
| Menon, P. K. |
RAPID PREDICTION OF AIR TRAFFIC FOR TRAJECTORY BASED OPERATIONS |
ICAS2008-11.6 ST (AIAA 2008-8902) |
| Menon, P. K. |
TRAJECTORY UNCERTAINTY MODELING FOR QUEUEING ANALYSIS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.1.1 (AIAA 2008-8854) |
| Merazzi, S. |
UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
| Mercer, J. |
CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
| Mercer, J. |
HUMAN-IN-THE-LOOP EVALUATION OF GROUND-BASED AUTOMATED SEPARATION ASSURANCE FOR NEXTGEN |
ICAS 2008-11.4.5 (AIAA 2008-8885) |
| Mermet-Guyennet, M. |
RELIABILITY STUDY OF POWER MODULE BY STOCHASTIC UNCERTAINTY METHOD FOR AN AERONAUTICAL APPLICATION |
ICAS 2008-6.1.1 |
| Meuret, R. |
HIGH EFFICIENCY, HIGH RELIABILITY 2 KW INVERTER FOR AERONAUTICAL APPLICATION |
ICAS 2008-6.1.3 |
| Meuret, R. |
RELIABILITY STUDY OF POWER MODULE BY STOCHASTIC UNCERTAINTY METHOD FOR AN AERONAUTICAL APPLICATION |
ICAS 2008-6.1.1 |
| Meussen, M. |
LONG TERM AIRCRAFT PROJECT AND TECHNOLOGY EVALUATION UNDER THE UNCERTAINTY OF FUTURE SCENARIOS |
ICAS 2008-1.3.4 |
| Micol, A. |
RELIABILITY STUDY OF POWER MODULE BY STOCHASTIC UNCERTAINTY METHOD FOR AN AERONAUTICAL APPLICATION |
ICAS 2008-6.1.1 |
| Miller, M. E. |
NETWORK ENABLED OPERATIONS ENHANCES AVIATION EFFICIENCY |
ICAS 2008-8.8.1 (AIAA 2008-8951) |
| Min, B. M. |
PERFORMANCE EVALUATION AND HILS TEST OF CONTROL ALLOCATION METHODS FOR RECONFIGURATION CONTROL |
ICAS 2008-5.10.3 |
| Miquel, T. |
MODIFIED BEZIER CURVE FOR 4D REFERENCE TRAJECTORY DEFINITION UNDER FLIGHT PROFILE CONSTRAINT |
ICAS 2008-11.6.3 (AIAA 2008-8900) |
| Miranda, G. |
3D OBSTACLE AVOIDANCE STRATEGIES FOR UAS (UNINHABITED AERIAL SYSTEMS) MISSION PLANNING AND RE-PLANNING |
ICAS 2008-5.6.1 (AIAA 2008-8962) |
| Mirzoyan, A. A. |
STUDIES ON MDO OF ENGINE DESIGN PARAMETERS WITH MISSION, NOISE & EMISSION CRITERIA AT SSBJ ENGINE CONCEPTUAL DESIGN |
ICAS 2008-4.2.3 |
| Mistry, S. |
NOVEL DESIGN CONCEPTS FOR AIRCRAFT WITH REDUCED NOISE AND GLOBAL WARMING CHARACTERISTICS |
ICAS 2008-4.10.4 |
| Moccia, A. |
DEVELOPMENT AND TEST OF AN INTEGRATED SENSOR SYSTEM FOR AUTONOMOUS COLLISION AVOIDANCE |
ICAS2008-P6.12 |
| Mohamed, K. |
KRYLOV RECYCLING TECHNIQUES FOR UNSTEADY SIMULATION OF TURBULENT AERODYNAMIC FLOWS |
ICAS2008-2.1 ST: |
| Möhlenbrink, C. |
AUGMENTED VISION VIDEOPANORAMA SYSTEM FOR REMOTE AIRPORT TOWER OPERATION |
ICAS 2008-8.3.1 |
| Moir, S. |
AERODYNAMIC STALL SUPPRESSION ON AEROFOIL SECTIONS USING PASSIVE AIR JET VORTEX GENERATORS |
ICAS 2008-3.11.3 |
| Monclar, P. |
LATEST DEVELOPMENTS IN ELECTRIAL LANDING SYSTEMS |
ICAS 2008-6.5.3 |
| Mondali, M. |
AN ANALYTICAL MODEL FOR PREDICTION OF THE STEADY STATE CREEP DEFORMATIONS AND STRESSES OF SHORT FIBER COMPOSITES |
ICAS 2008-9.8.3 |
| Montgomery, J. |
ENVIRONMENTALLY PROGRESSIVE AIRPLANES THROUGH AN INTEGRATED DESIGN FOR INTERIOR NOISE |
ICAS 2008-4.9.1 INVITED |
| Montoya, J. |
AN OPTIMIZATION MODEL FOR REDUCING AIRCRAFT TAXI TIMES AT THE DALLAS-FORT WORTH INTERNATIONAL AIRPORT |
ICAS 2008-8.6.1 |
| Moore, D. P. |
147 THE LOW DOWN – DIGITAL TERRAIN DATA FOR AUTOMATIC GROUND COLLISION AVOIDANCE |
ICAS2008-P6.10 |
| Moorhouse, D. |
NUMERICAL STUDY OF ENERGY UTILIZATION IN NOZZLE/PLUME FLOW-FIELDS OF HIGH-SPEED AIR-BREATHING VEHICLES |
ICAS 2008-4.3.3 |
| Mora-Camino, F. |
MODIFIED BEZIER CURVE FOR 4D REFERENCE TRAJECTORY DEFINITION UNDER FLIGHT PROFILE CONSTRAINT |
ICAS 2008-11.6.3 (AIAA 2008-8900) |
| Morgado Belo, E. M. |
INFLUENCES INVESTIGATION OF NUMERICAL PARAMETERS AND MESHING ON THE AEROELASTIC RESPONSE |
ICAS2008- P3.4 |
| Morgado Belo, E. M. |
NUMERICAL DEVELOPMENT OF A FLUTTER ACTIVE CONTROL SYSTEM BASED ON PRESSURE FEEDBACK. |
ICAS2008-P3.3 |
| Mori, R. |
NEURAL NETWORK ANALYSIS OF PILOT MANEUVER DURING LANDING PHASE |
ICAS 2008-5.4.4 |
| Morris, A. M. |
TOWARDS AERODYNAMIC OPTIMISATION OF AN AEROELASTIC WING USING DOMAIN ELEMENT PARAMETERISATION |
ICAS 2008-2.8.1 |
| Morrow, C. |
SIMULTANEOUS IMPROVEMENTS IN ENVIRONMENTAL PERFORMANCE AND OPERATIONAL EFFICIENCY ENABLED BY SIGNIFICANTLY QUIETER AIRCRAFT |
ICAS 2008-11.2.2 (AIAA 2008-8858) |
| Motamedian, H. R. |
MICROMECHANICAL FEM MODELING OF THERMAL STRESSES IN FUNCTIONALLY GRADED MATERIALS |
ICAS 2008-7.2.4 |
| Motogoe, S. |
ESTIMATION OF THE INFLUENCE OF PROFILE ERROR ON AERODYNAMIC PERFORMANCE FOR LOW-REYNOLDS-NUMBER AIRFOILS |
ICAS2008-3.7 ST: |
| Muehlhausen, T. |
THE USE OF MODELS FOR ATM VALIDATION: FROM AIRPORT EXTENSION PROGRAMS TO THE AIR TRANSPORT SYSTEM OF THE FUTURE |
ICAS2008-8.9 ST: |
| Mueller, B. E. |
METHODOLOGY FOR THERMALLY INDUCED LOADING IN STRUCTURAL ANALYSIS ON THE F-35 LIGHTNING II |
ICAS 2008-7.11.1 |
| Mueller, E. |
FLIGHT DECK PROCEDURAL GUIDELINES FOR DATALINK TRAJECTORY NEGOTIATIONS |
ICAS 2008-11.6.4 (AIAA 2008-8901) |
| Muffo, D. |
COMPRESSIBLE FLUID-FLOW ALE FORMULATION ON CHANGING TOPOLOGY MESHES FOR AEROELASTIC SIMULATIONS |
ICAS2008-2.10 ST: |
| Mulder, M. |
FEASIBILITY ANALYSIS OF ACHIEVING A STABILIZED APPROACH |
ICAS 2008-5.4.2 |
| Mulder, T. J. |
ON THE REDUCTION OF NOX-EMISSION LEVELS BY PERFORMING LOW NOX FLIGHTS |
ICAS2008-4.7 ST: |
| Mullan, M. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
| Mulyanto, T. |
643 DEVELOPMENT OF A COAXIAL ROTOR MAV FOR INDOOR APPLICATION |
ICAS2008-P1.9 |
| Mundra, A. D. |
SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
| Murayama, M. |
COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA |
ICAS 2008-2.2.1 |
| Murayama, M. |
INVESTIGATION OF THE FLOW OVER NACELLE/PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION |
ICAS 2008-3.3.3 |
| Murdoch, J. L. |
OPERATIONAL IMPROVEMENTS FROM IN-TRAIL PROCEDURE IN THE NORTH ATLANTIC ORGANIZED TRACK SYSTEM |
ICAS 2008-11.6.1 (AIAA 2008-8898) |
| Murdoch, J. L. |
PILOT IN-TRAIL PROCEDURE VALIDATION SIMULATION STUDY |
ICAS 2008-10.5.2 (AIAA 2008-8896) |
| Murphy, D. |
THE MODERNIZED NATIONAL AIRSPACE SYSTEM PERFORMANCE ANALYSIS CAPABILITY (NASPAC) |
ICAS 2008-9.11.2 (AIAA 2008-8945) |
| Musaj, M. |
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THE AERODYNAMICS OF UNCONVENTIONAL W-LEADING EDGE REVERSED DELTA WING IN GROUND EFFECT |
ICAS 2008-3.5.3 |
| Myerscough, K. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
| Nadarajah, S. |
KRYLOV RECYCLING TECHNIQUES FOR UNSTEADY SIMULATION OF TURBULENT AERODYNAMIC FLOWS |
ICAS2008-2.1 ST: |
| Nadot, Y. |
FATIGUE DESIGN OF METALLIC COMPONENTS CONTAINING SURFACE OR INTERNAL DEFECTS |
ICAS 2008-7.4.3 |
| Nadot-Martin, C. |
A MULTI-SCALE “MORPHOLOGICAL APPROACH” FOR MODELING THE NON LINEAR BEHAVIOR OF PROPELLANT-LIKE MATERIALS |
ICAS 2008-7.1.3 |
| Nag, M. |
TRAJECTORY UNCERTAINTY MODELING FOR QUEUEING ANALYSIS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.1.1 (AIAA 2008-8854) |
| Nagai, H. |
EXPERIMENTAL STUDY ON INTERFERENCE FLOW OF A SUPERSONIC BUSEMANN BIPLANE USING PRESSURE-SENSITIVE PAINT TECHNIQUE |
ICAS 2008-3.7.5 |
| Nagai, H. |
MEASUREMENT OF UNSTEADY AERODYNAMIC FORCES OF 3D FLAPPING WING IN HOVERING TO FORWARD FLIGHT |
ICAS 2008-3.4.3 |
| Nagai, K. |
AERODYNAMIC DESIGN AND ITS VALIDATION OF AN OPEN-TYPE ENGINE RUN-UP FACILITY |
ICAS 2008-4.5.3 |
| Nagaoka, S. |
A MODEL FOR ESTIMATING THE LATERAL OVERLAP PROBABILITY OF AIRCRAFT WITH RNP ALERTING CAPABILITY IN PARALLEL RNAV ROUTES |
ICAS 2008-9.7.5 |
| Nagaoka, S. |
ANALYSIS OF GAPS BETWEEN THE PREDICTIVE AND THE ADAPTIVE COMPONENT IN ATM |
ICAS 2008-11.10.2 (AIAA 2008-8941) |
| Nagasaka, N. |
AUTONOMOUS AERIAL OBSERVATION SYSTEM FOR DISASTER RESPONSE USING ELECTRIC DUCTED FAN MAVS |
ICAS 2008-1.4.5 |
| Nagel, B. |
ACTIVE AND PASSIVE STRUCTURAL MEASURES FOR AEROELASTIC WINGLET DESIGN |
ICAS 2008-7.10.1 |
| Nagy, A. |
INVESTIGATION ON THE EFFECT OF HYDRODYNAMIC MEMS ON AIRFOIL |
ICAS2008-3.10 ST: |
| Nakahashi, K. |
MULTI-DISCIPLINARY DESIGN EXPLORATION FOR WINGLET |
ICAS 2008-1.1.3 |
| Nakakita, K. |
TRANSONIC FLUTTER WIND TUNNEL TESTS OF CONVENTIONAL TWIN-ENGINE TRANSPORT SEMISPAN MODEL |
ICAS 2008-9.6.2 |
| Nakamichi, J. |
TRANSONIC FLUTTER WIND TUNNEL TESTS OF CONVENTIONAL TWIN-ENGINE TRANSPORT SEMISPAN MODEL |
ICAS 2008-9.6.2 |
| Nangia, R. K. |
ACHIEVING HIGHLY EFFICIENT CIVIL AVIATION - WHY & HOW WITH AIR-TO-AIR REFUELLING, REVIEW & NEW DEVELOPMENTS |
ICAS 2008-4.10.1 |
| Nangia, R. K. |
SUPERSONIC AIRCRAFT FORMATION FLYING TO INCREASE FLIGHT EFFICIENCY |
ICAS 2008-1.10.2 |
| Nardin, L. |
AERODYNAMIC OPTIMIZATION OF AIRCRAFT CONFIGURATIONS WITH MULTIDISZIPLINARY ASPECTS |
ICAS 2008-2.11.3 |
| Narkiewicz, J. P. |
NONLINEAR MODEL FOLLOWING RECONFIGURABLE FLIGHT CONTROL SYSTEM |
ICAS 2008-5.10.4 |
| Naruoka, M. |
ATTITUDE ACCURACY IMPROVEMENT OF ULTRA LOW-GRADE MEMS INS USING ALIGNMENT OF GPS ANNTENA |
ICAS2008-P6.11 |
| Natan, B. |
PULSATING COMBUSTION OF AN ORGANIC GEL-FUEL DROPLET AND ITS INFLUENCE ON THE THERMAL FIELD OF A SPRAY DIFFUSION FLAME |
ICAS 2008-4.1.2 |
| Navazi, H. M. |
SCALED DOWN MODELS FOR FREE VIBRATION ANALYSIS OF ORTHOGONALLY STIFFENED CYLINDRICAL SHELLS USING SIMILITUDE THEORY |
ICAS 2008-7.7.5 |
| Négrier, J. |
DESIGN OF A SMALL SUPERSONIC TRANSPORT AIRCRAFT WITH HIGH ENVIRONMENTAL CONSTRAINTS |
ICAS 2008-1.10.1 INVITED |
| Nejjari, F. |
HIERARCHICAL AND SENSITIVITY ANALYSIS FOR NOISE ABATEMENT DEPARTURE PROCEDURES |
ICAS 2008-11.3.3 (AIAA 2008-8867) |
| Nelson, R. C. |
FOREBODY VORTEX CONTROL ON HIGH PERFORMANCE AIRCRAFT USING PWM-CONTROLLED PLASMA ACTUATORS |
ICAS 2008-3.3.4 |
| Nesterenko, B. G. |
ESTIMATION OF CRACK TURN PHENOMENON |
ICAS 2008-7.6.3 |
| Nesterenko, G. I. |
ESTIMATION OF CRACK TURN PHENOMENON |
ICAS 2008-7.6.3 |
| Ng, A. |
SUITABILITY OF DIFFERENT CRACK GROWTH MODELS FOR ANALYSING MULTI-SITE DAMAGE IN AIRCRAFT STRUCTURAL CONFIGURATIONS |
ICAS2008-7.6 ST: |
| Nguyen Van, T. |
SYSTEM INFRASTRUCTURE FOR INTEGRATED AND COLLABORATIVE PRODUCT DEVELOPMENT IN THE AERONAUTIC INDUSTRY |
ICAS 2008-6.10.2 |
| Nibourg, J. M. |
ENVIRONMENT-AWARE RUNWAY ALLOCATION ADVICE SYSTEM |
ICAS 2008-4.11.2 |
| Nicolosi, F. |
DESIGN AND AERODYNAMIC ANALYSIS OF A LIGHT TWIN ENGINE PROPELLER AIRCRAFT |
ICAS 2008-1.2.2 |
| Nicolosi, F. |
SINGLE VERSUS MULTIPLE WINGLETS: NUMERICAL AND EXPERIMENTAL INVESTIGATION |
ICAS 2008-2.7.3 |
| Niedringhaus, W. P. |
USING AIRSPACEANALYZER TO EFFICIENTLY PROVIDE SPACING FOR AIRCRAFT ACROSS MULTIPLE SECTORS |
ICAS 2008-11.2.4 (AIAA 2008-8860 ) |
| Niesner, R. |
NUMERICAL ANALYSIS OF THIN-WALLED STRUCTURES IN HYPERSONIC FLOW REGIME |
ICAS 2008-3.6.1 |
| Nigmatullin, R. Z. |
UNSTEADY CFD MODELING OF WHOLE GAS TURBINE ENGINE FLOW PASSAGE WITH APPLICATIONS |
ICAS2008-4.4 ST: |
| Nitsche, W. |
A WALL SHEAR STRESS MEASUREMENT TECHNIQUE USING THE THERMAL WAKES OF SMALL HEATED SPOTS |
ICAS 2008-3.7.1 |
| Nitsche, W. |
ACTIVE CANCELLATION OF TOLLMIEN-SCHLICHTING INSTABILITIES UP TO M = 0.40 |
ICAS 2008-3.10.2 |
| Nitsche, W. |
ACTIVE SEPARATION CONTROL ON A SLATLESS 2D HIGH-LIFT WING SECTION |
ICAS 2008-3.11.2 |
| Nitsche, W. |
IN-FLIGHT EXPERIMENTS FOR DELAYING LAMINAR-TURBULENT TRANSITION ON A LAMINAR WING GLOVE |
ICAS 2008-3.7.3 |
| Noda, F. |
CBAQ: DEVELOPMENT OF CRM BEHAVIOR ANALYSIS METHOD FOR MISSION FLIGHT CREW TRAINING |
ICAS 2008-9.2.1 |
| Noguchi, M. |
NUMERICAL STUDY OF A PITOT PROBE WITH FIVE-HOLE PYRAMIDAL HEAD FOR SUPERSONIC FLIGHT TEST |
ICAS 2008-3.2.4 |
| Noonan, K. |
NATSIM: A SYSTEMS DYNAMICS MODEL OF NORTH ATLANTIC AIR TRAFFIC |
ICAS 2008-9.11.3 (AIAA 2008-8912) |
| Noonan, K. |
THE MODERNIZED NATIONAL AIRSPACE SYSTEM PERFORMANCE ANALYSIS CAPABILITY (NASPAC) |
ICAS 2008-9.11.2 (AIAA 2008-8945) |
| Noordman, B. A. T. |
OPTIMISING HIGH-EFFICIENCY RUDDERS FOR TRANSPORT AIRCRAFT FUEL BURN REDUCTION |
ICAS 2008-2.11.2 |
| Nozicka, J. |
SEPARATION CONTROL BY SYNTHETIC JET ACTUATOR IN STRAIGHT BLADE CASCADE |
ICAS 2008-3.10.4 |
| Obayashi, S. |
WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION |
ICAS2008-2.4 ST: |
| Ochieng, W. |
SATELLITE-BASED NAVIGATION ARCHITECTURE STUDY FOR AIRCRAFT CATEGORY III LANDINGS |
ICAS 2008-6.4.4 |
| Ogawa, T. |
EXPERIMENTAL STUDY ON INTERFERENCE FLOW OF A SUPERSONIC BUSEMANN BIPLANE USING PRESSURE-SENSITIVE PAINT TECHNIQUE |
ICAS 2008-3.7.5 |
| Ogawa, T. |
WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION |
ICAS2008-2.4 ST: |
| Oheimb, D. von |
SECURITY ARCHITECTURE AND FORMAL ANALYSIS OF AN AIRPLANE SOFTWARE DISTRIBUTION SYSTEM |
ICAS 2008-9.1.1 |
| Oliveira, G. L. |
A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
| Oliveira, J. M. G. S. |
ON THE EFFECTS ON NOISE OF GROUND REFLECTION AND ATMOSPHERIC ATTENUATION ON THE NOISE OF HELICOPTERS |
ICAS 2008-3.9.4 |
| Olsen, R. F. |
MODELING OF ACOUSTICALLY TREATED NACELLE LIP TRANSPIRATION FLOW ANTI-ICING SYSTEM |
ICAS 2008-6.4.3 |
| Olsson, P. -M. |
ROUTE PLANNING FOR RELAY UAV |
ICAS 2008-5.6.2 |
| Ölvander, J. |
A QUANTIFIED RELATIONSHIP MATRIX AIDED BY PROBABILISTIC DESIGN AND OPTIMIZATION |
ICAS 2008-6.2.1 |
| Omar, Z. |
GENETIC FUZZY CONTROL FOR AUTONOMOUS DUCTED-FAN VTOL UAV |
ICAS 2008-5.9.3 |
| Ommi, F. |
EXPERIMENTAL INVESTIGATION OF SPRAY CHARACTERISTICS OF DOUBLE-BASE SWIRL INJECTOR |
ICAS2008-4.1 ST: |
| Onorato, M. |
INVESTIGATION OF THE FLOW IN A RECTANGULAR CAVITY USING TOMOGRAPHIC AND TIME-RESOLVED PIV |
ICAS 2008-3.2.2 |
| Onorato, M. |
THE EFFECTS OF WALL ROUGHNESS ON THE TURBULENT BOUNDARY LAYER |
ICAS 2008-3.8.1 |
| Oppelstrup, J. |
CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
| Orchard, D. M. |
THE APPLICATION OF SEMI-EMPIRICAL STORE RELEASE SIMULATION FOR THE OPTIMIZATION OF GRID SURVEY WIND TUNNEL TESTING |
ICAS 2008-3.1.3 |
| Orieux, S. |
AUTOMATED GENERATION, SELECTION AND EVALUATION OF ARCHITECTURES FOR ELECTROMECHANICAL ACTUATORS |
ICAS 2008-6.6.1 |
| Orifici, A. C. |
THE DESIGN OF POSTBUCKLING COMPOSITE AEROSPACE STRUCTURES ACCOUNTING FOR DAMAGE INITIATION AND GROWTH |
ICAS 2008-7.3.2 |
| Ortiz, D. |
THE FEASIBILITY AND POTENTIAL ENVIRONMENTAL BENEFITS OF ALTERNATIVE FUELS FOR COMMERCIAL AVIATION |
ICAS 2008-4.7.5 |
| Ostwald, P. |
AIRSPACE SECURITY MEASURES EMPLOYED FOR THE UN GENERAL ASSEMBLY MEETING: ANALYSIS AND IMPACT |
ICAS 2008-11.5.1 (AIAA 2008-8892) |
| Ostwald, P. |
INTEGRATED TIME-BASED FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.10.1 (AIAA 2008-8940) |
| Owen, B. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
| Oyama, S. |
EXPERIMENTAL STUDY ON INTERFERENCE FLOW OF A SUPERSONIC BUSEMANN BIPLANE USING PRESSURE-SENSITIVE PAINT TECHNIQUE |
ICAS 2008-3.7.5 |
| Ozaki, S. |
WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION |
ICAS2008-2.4 ST: |
| Oztekin, A. |
HAZARD, SAFETY RISK AND UNCERTAINTY MODELING OF THE INTEGRATION OF UNMANNED AIRCRAFT SYSTEMS INTO THE NATIONAL AIRSPACE |
ICAS 2008-9.7.2 |
| Paglione, P. |
A PROCEDURE TO DESIGN AIRCRAFT FLIGHT CONTROL LAWS TAKING INTO ACCOUNT ROBUSTNESS USING THE VARIABLE STRUCTURE CONTROL |
ICAS2008-5.4 ST: |
| Paielli, R. A. |
TACTICAL CONFLICT RESOLUTION USING VERTICAL MANEUVERS IN ENROUTE AIRSPACE |
ICAS2008-11.4 ST (AIAA 2008-8886) |
| Pak, C. -G. |
STRUCTURAL MODEL TUNING CAPABILITY IN AN OBJECT-ORIENTED MULTIDISCIPLINARY DESIGN, ANALYSIS, AND OPTIMIZATION TOOL |
ICAS 2008-9.5.1 |
| Pak, C.-G. |
MULTIDISCIPLINARY DESIGN, ANALYSIS, AND OPTIMIZATION TOOL DEVELOPMENT USING GENETIC ALGORITHM |
ICAS 2008-1.1.1 |
| Palaniappan, K. |
TRAJECTORY UNCERTAINTY MODELING FOR QUEUEING ANALYSIS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.1.1 (AIAA 2008-8854) |
| Palmer, E. |
CONTROLLER SUPPORT FOR MANAGING HIGH-EFFICIENCY ARRIVALS IN DENSE TRAFFIC ENVIRONMENTS |
ICAS 2008-11.10.4 (AIAA 2008-8943) |
| Palmer, M. E. |
SUPERSONIC AIRCRAFT FORMATION FLYING TO INCREASE FLIGHT EFFICIENCY |
ICAS 2008-1.10.2 |
| Pant, R. |
INCLUSION OF ENGINE RELATED PARAMETERS IN CONCEPTUAL DESIGN OF MORPHING AIRCRAFT |
ICAS 2008-1.6.4 |
| Pant, R. S. |
DESIGN, FABRICATION AND OPERATION OF REMOTELY CONTROLLED AIRSHIPS IN INDIA |
ICAS 2008-10.1.3 (AIAA 2008-8853) |
| Pant, R. S. |
LOW COST TRANS-RIVER AERIAL-FERRY USING A NOVEL LTA SYSTEM |
ICAS 2008-10.1.2 (AIAA 2008-8851) |
| Paraschivoiu, M. |
KRYLOV RECYCLING TECHNIQUES FOR UNSTEADY SIMULATION OF TURBULENT AERODYNAMIC FLOWS |
ICAS2008-2.1 ST: |
| Parekh, D. |
DESIGN OF A NOVEL INTELLIGENT DATA MANAGEMENT TOOL FOR HEALTH AND USAGE MONITORING SYSTEMS – DESIGN REQUIREMENTS |
ICAS2008-6.1 ST: |
| Parezanovic, V. |
ON AIRCRAFT PERFORMANCE IMPROVEMENT BY USING WINGLETS |
ICAS 2008-2.8.3 |
| Park, H. -U. |
A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
| Pascale, L. |
DESIGN AND AERODYNAMIC ANALYSIS OF A LIGHT TWIN ENGINE PROPELLER AIRCRAFT |
ICAS 2008-1.2.2 |
| Pastorelli, S. |
FLY-BY-WIRE CONTROL OF A HELICOPTER: MULTIBODY MAIN ROTOR MODEL |
ICAS2008-5.11 ST: |
| Patek, Z. |
PERFORMANCE DEGRADATION OF A SIMULATED ICE CONTAMINATED AIRFOIL BY SUPER-COOLED DROPLETS |
ICAS 2008-3.7.2 |
| Pátek, Z. |
WIND TUNNEL AND COMPUTIONAL INVESTIGATION OF SIMULATED CONTAMINATION ON AIRFOIL |
ICAS2008-P2.11 |
| Patel, C. K. |
THEORETICAL AND EXPERIMENTAL INVESTIGATION OF ENERGY EXTRACTION FROM ATMOSPHERIC TURBULENCE |
ICAS2008-1.5 ST: |
| Pätzold, A. |
IN-FLIGHT EXPERIMENTS FOR DELAYING LAMINAR-TURBULENT TRANSITION ON A LAMINAR WING GLOVE |
ICAS 2008-3.7.3 |
| Paul, D. |
FLIGHT VEHICLE COMPOSITE STRUCTURES |
ICAS 2008-7.9.1 (AIAA 2008-8976 ) |
| Paull, G. |
OPERATIONAL ASSESSMENT OF THE INTEGRATED TERMINAL WEATHER SYSTEM (ITWS) USING DIRECT MEASUREMENT |
ICAS 2008-10.7.5 (AIAA 2008-8918) |
| Pe, T. |
MULTIVARIABLE CONTROLLER DESIGN FOR A TRIMMABLE HORIZONTAL STABILIZER ACTUATOR WITH TWO PRIMARY LOAD PATHS |
ICAS 2008-6.4.2 |
| Pechloff, A. |
SMALL DISTURBANCE NAVIER-STOKES COMPUTATIONS FOR LOW ASPECT RATIO WING PITCHING OSCILLATIONS |
ICAS 2008-2.10.3 |
| Peigin, S. |
EFFICIENT APPROACH FOR MULTIPOINT AERODYNAMIC WING DESIGN OF BUSINESS JET AIRCRAFT |
ICAS 2008-2.11.1 |
| Peigin, S. |
HYBRIDIZATION OF HETEROGENEOUS 3D CFD DISCRETIZATIONS VIA DIRECT FLUX OPTIMIZATION |
ICAS2008-2.3 ST: |
| Peltzer, I. |
ACTIVE SEPARATION CONTROL ON A SLATLESS 2D HIGH-LIFT WING SECTION |
ICAS 2008-3.11.2 |
| Peltzer, I. |
IN-FLIGHT EXPERIMENTS FOR DELAYING LAMINAR-TURBULENT TRANSITION ON A LAMINAR WING GLOVE |
ICAS 2008-3.7.3 |
| Peraire, J. |
COMPUTATIONAL INVESTIGATION AND DESIGN OF COMPLIANT MEMBRANE WINGS FOR BIOLOGICALLY INSPIRED FLIGHT VEHICLES |
ICAS 2008-2.10.1 |
| Perebatov, V. |
THEORETICAL APPROACH TO DIRECTIONAL CONTROL SENSITIVITY SELECTION |
ICAS 2008-5.4.1 INVITED |
| Pereira, G. A. S. |
DEVELOPMENT OF A SMALL UNMANNED AIR VEHICLE WITH MINIMUM SENSORS PHILOSOPHY |
ICAS2008-1.4 ST: |
| Pereira, N. C. |
APPLICATION OF A MODEL UPDATING METHOD TO AN AIRCRAFT LONGITUDINAL STABILITY AUGMENTATION SYSTEM |
ICAS2008-5.2 ST: |
| Perez, E. |
AIRPLANE DESIGN: A MUST IN AERONAUTICAL ENGINEERING EDUCATION |
ICAS2008-P1.6 |
| Persiani, F. |
3D OBSTACLE AVOIDANCE STRATEGIES FOR UAS (UNINHABITED AERIAL SYSTEMS) MISSION PLANNING AND RE-PLANNING |
ICAS 2008-5.6.1 (AIAA 2008-8962) |
| Persiani, F. |
A NEW AIRCRAFT CONCEPT: THE COMBAT MALE |
ICAS 2008-1.4.4 |
| Persiani, F. |
DESIGN AND DEVELOPMENT OF AN ATC DISTRIBUTED TRAINING SYSTEM |
ICAS2008-P8.2 (AIAA 2008-8873) |
| Persiani, F. |
DESIGN AND EVALUATION OF A 4D INTERFACE FOR ATC |
ICAS 2008-9.10.3 |
| Persson, I. |
TRANSONIC STORE SEPARATION STUDIES ON THE SAAB GRIPEN AIRCRAFT USING COMPUTATIONAL AERODYNAMICS |
ICAS 2008-2.9.1 |
| Pesak, M. |
OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING - EXPERIMENTAL VERIFICATION |
ICAS 2008-9.5.2 |
| Pezzella, G. |
ANALYSIS OF THERMOCHEMICAL MODELING AND SURFACE CATALYTICITY IN SPACE VEHICLES REENTRY |
ICAS 2008-3.6.2 |
| Pfaender, H. |
A METHOD FOR ASSESSING THE ENVIRONMENTAL BENEFIT OF FUTURE AVIATION TECHNOLOGIES |
ICAS2008-P10.2 |
| Pfeiffer, U. |
IMPACT RESISTANCE, DAMAGE TOLERANCE AND NON-DESTRUCTIVE DAMAGE DETECTION FOR SANDWICH STRUCTURES: ANALYSIS AND TESTING |
ICAS2008-7.5 ST: |
| Phan, L. |
PARAMETRIC MODELING OF AN ELECTRICAL TEST RIG FOR POWER OPTIMIZED AIRCRAFT ARCHITECTURES |
ICAS2008-6.6 ST (AIAA 2008-8973) |
| Phleps, P. |
IMPACT OF ESTOL CAPABILITY ON RUNWAY CAPACITY - AN ANALYTICAL APPROACH |
ICAS 2008-11.9.4 (AIAA 2008-8933) |
| Piekert, F. |
OPERATIONAL CONCEPT FOR AN AIRPORT OPERATIONS CENTER TO ENABLE TOTAL AIRPORT MANAGEMENT |
ICAS 2008-8.3.2 |
| Pierce, R. S. |
COMPARING SITUATION AWARENESS MEASUREMENT TECHNIQUES IN A LOW FIDELITY AIR TRAFFIC CONTROL SIMULATION |
ICAS 2008-9.7.4 |
| Pinon, O. |
A METHODOLOGICAL APPROACH FOR AIRPORT TECHNOLOGY EVALUATION AND SELECTION |
ICAS 2008-8.3.4 (AIAA 2008-8965) |
| Pires, M. |
TURBULENCE MODELING S AND APPLICATIONS TO AEROSPIKE PLUG NOZZLE |
ICAS 2008-4.1.3 |
| Pistek, A. |
OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING - EXPERIMENTAL VERIFICATION |
ICAS 2008-9.5.2 |
| Pittofrati, M. |
SURVEY OF FEASIBLE NUMERICAL APPROACHES TO ANALYSE THE BEHAVIOUR OF A COMPOSITE SKIN PANEL DURING A WATER IMPACT |
ICAS 2008-7.9.2 |
| Pizzolo, A. |
TRAJECTORY TRACKING FOR A NON - CONVENTIONAL UAV |
ICAS2008-P5.3 |
| Plágaro, L. |
AERODYNAMIC OPTIMIZATION OF A BLENDED WING BODY |
ICAS2008-2.11 ST: |
| Platzer, M. F. |
FLAPPING-WING TECHNOLOGY: THE POTENTIAL FOR AIR VEHICLE PROPULSION AND AIRBORNE POWER GENERATION |
ICAS 2008-1.5.1 |
| Plegas, P. |
VIRTUAL ENTERPRISE COLLABORATION - BREAKTHROUGH TECHNOLOGIES PROVIDED BY VIVACE |
ICAS 2008-8.10.4 INVITED |
| Ploetner, K. O. |
INVESTIGATION OF LONG-HAUL FLIGHT ATTRIBUTES INFLUENCING PASSENGER'S BOOKING DECISION USING SP DATA |
ICAS 2008-6.3.1 |
| Pointon, J. M. |
THERMAL MANAGEMENT OF ELECTROMECHANICAL ACTUATION ON AN ALL-ELECTRIC AIRCRAFT |
ICAS 2008-6.6.2 |
| Poovendran, R. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
| Poovendran, R. |
SECURITY OF WIRELESS SENSOR NETWORK ENABLED HEALTH MONITORING FOR FUTURE AIRPLANES |
ICAS 2008-9.1.3 |
| Popelka, L. |
SEPARATION CONTROL BY SYNTHETIC JET ACTUATOR IN STRAIGHT BLADE CASCADE |
ICAS 2008-3.10.4 |
| Poppe, M. |
TOWARDS SESAR PERFORMANCE TARGETS - THE SUPER-HIGHWAY APPROACH |
ICAS 2008-10.10.1 (AIAA 2008-8935) |
| Porter, D. J. |
SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
| Post, J. |
NATSIM: A SYSTEMS DYNAMICS MODEL OF NORTH ATLANTIC AIR TRAFFIC |
ICAS 2008-9.11.3 (AIAA 2008-8912) |
| Post, J. |
THE MODERNIZED NATIONAL AIRSPACE SYSTEM PERFORMANCE ANALYSIS CAPABILITY (NASPAC) |
ICAS 2008-9.11.2 (AIAA 2008-8945) |
| Post, M. |
FLIGHT EVALUATION OF A COMPACT AIRBORNE TRACE GAS ANALYSIS SENSOR PROOF-OF-CONCEPT |
ICAS2008-P6.4 |
| Prananta, B. B. |
EFFICIENT AEROELASTIC SIMULATION IN A PARAMETRIC PROCEDURE FOR FATIGUE ANALYSIS |
ICAS 2008-7.7.1 |
| Prats, X. |
HIERARCHICAL AND SENSITIVITY ANALYSIS FOR NOISE ABATEMENT DEPARTURE PROCEDURES |
ICAS 2008-11.3.3 (AIAA 2008-8867) |
| Pratt, D. |
FLIGHT VEHICLE COMPOSITE STRUCTURES |
ICAS 2008-7.9.1 (AIAA 2008-8976 ) |
| Preatoni, M. L. |
FLIGHT MECHANICS SIMULATOR FOR ROTORCRAFT DEVELOPMENT |
ICAS2008-P5.4 |
| Prete, J. |
CAUSALITY ANALYSIS FOR AVIATION WEATHER HAZARDS |
ICAS 2008-10.7.1 (AIAA 2008-8914) |
| Prete, J. |
ON-DEMAND SPECIAL USE AIRSPACE |
ICAS 2008-10.10.4 (AIAA 2008-8938) |
| Prete, J. |
PRINCIPLES OF AIRSPACE TUBE DESIGN FOR DYNAMIC AIRSPACE CONFIGURATION |
ICAS 2008-10.10.5 (AIAA 2008-8939) |
| Prevot, T. |
HUMAN-IN-THE-LOOP EVALUATION OF GROUND-BASED AUTOMATED SEPARATION ASSURANCE FOR NEXTGEN |
ICAS 2008-11.4.5 (AIAA 2008-8885) |
| Prince, S. A. |
AERODYNAMIC STALL SUPPRESSION ON AEROFOIL SECTIONS USING PASSIVE AIR JET VORTEX GENERATORS |
ICAS 2008-3.11.3 |
| Prince, S. A. |
AN EXPERIMENTAL AND COMPUTATIONAL COMPARISON OF THE LOW SPEED AERODYNAMICS OF SQUARE AND CIRCULAR SECTIONED BODIES |
ICAS2008-3.5 ST: |
| Prince, S. A. |
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THE AERODYNAMICS OF UNCONVENTIONAL W-LEADING EDGE REVERSED DELTA WING IN GROUND EFFECT |
ICAS 2008-3.5.3 |
| Prince, S. A. |
VORTEX SHEDDING FROM A ROTATING CIRCULAR CYLINDER AT MODERATE SUB-CRITICAL REYNOLDS NUMBERS AND HIGH VELOCITY RATIO |
ICAS 2008-3.10.5 |
| Prisell, E. |
A STUDY OF AN USER AND ENVIRONMENTAL FRIENDLY STORED ENERGY BASED EPU/APU-SYSTEM FOR MILITARY AEROSPACE APPLICATIONS |
ICAS 2008-6.4.5 |
| Pronk, F. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
| Przytula, K. W. |
HEALTH MONITORING FOR COMMERCIAL AIRCRAFT SYSTEMS |
ICAS 2008-6.1.2 |
| Puig, V. |
HIERARCHICAL AND SENSITIVITY ANALYSIS FOR NOISE ABATEMENT DEPARTURE PROCEDURES |
ICAS 2008-11.3.3 (AIAA 2008-8867) |
| Qiao, Z. D. |
LIFT PREDICTION OF MULTI-ELEMENT AIRFOIL USING DES AND RANS |
ICAS2008-P2.5 |
| Qiao, Z. D. |
RESEARCH ON MONITORING AND CONTROL SYSTEM BASED PLC IN THE NF-6 WIND TUNNEL |
ICAS2008-P2.10 |
| Qiao, Z. H. D. |
AERODYNAMIC SHAPE OPTIMIZATION OF TRANSONIC AEROELASTIC WING BASED ON CONTROL THEORY |
ICAS2008-9.6 ST: |
| Qiao, Z.D. |
TRANSONIC FLUTTER ANALYSIS OF AN AIRFOIL WITH APPROXIMATE BOUNDARY METHOD |
ICAS 2008-7.10.5 |
| Quagliotti, F. |
TRAJECTORY OPTIMISATION FOR AUTONOMOUS VEHICLES: A MINIUAV APPLICATION |
ICAS 2008-5.6.3 |
| Quaranta, G. |
BIOMECHANICAL PILOT PROPERTIES IDENTIFICATION BY INVERSE KINEMATICS/INVERSE DYNAMICS MULTIBODY ANALYSIS |
ICAS 2008-9.10.4 |
| Quaranta, G. |
COMPRESSIBLE FLUID-FLOW ALE FORMULATION ON CHANGING TOPOLOGY MESHES FOR AEROELASTIC SIMULATIONS |
ICAS2008-2.10 ST: |
| Quest, J. |
DEVELOPMENT & APPLICATION OF MODERN MEASUREMENT TECHNIQUES FOR PRESSURIZED CRYOGENIC WIND TUNNELS |
ICAS 2008-3.2.1 |
| Quevedo, J. |
HIERARCHICAL AND SENSITIVITY ANALYSIS FOR NOISE ABATEMENT DEPARTURE PROCEDURES |
ICAS 2008-11.3.3 (AIAA 2008-8867) |
| Rachami, J. |
SIMULTANEOUS IMPROVEMENTS IN ENVIRONMENTAL PERFORMANCE AND OPERATIONAL EFFICIENCY ENABLED BY SIGNIFICANTLY QUIETER AIRCRAFT |
ICAS 2008-11.2.2 (AIAA 2008-8858) |
| Radespiel, R. |
A COMPARISON OF NUMERICAL RANS SIMULATIONS AND FLOW FIELD MEASUREMENTS OF AN OSCILLATING AIRFOIL FOR FLAPPING WING PROPULSION |
ICAS 2008-2.10.2 |
| Ragazzi, A. |
FLIGHT MECHANICS SIMULATOR FOR ROTORCRAFT DEVELOPMENT |
ICAS2008-P5.4 |
| Raghunathan, S. |
EXCRESCENCES EFFECTS IN AERODYNAMICS |
ICAS2008-3.8 ST: |
| Raghunathan, S. |
LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
| Raina, A. A. |
DESIGN, FABRICATION AND OPERATION OF REMOTELY CONTROLLED AIRSHIPS IN INDIA |
ICAS 2008-10.1.3 (AIAA 2008-8853) |
| Raina, A. A. |
LOW COST TRANS-RIVER AERIAL-FERRY USING A NOVEL LTA SYSTEM |
ICAS 2008-10.1.2 (AIAA 2008-8851) |
| Ramesh, A. |
ADVANCED METHODOLOGIES FOR AVERAGE PROBABILITY CALCULATION FOR AEROSPACE SYSTEMS |
ICAS 2008-9.3.3 |
| Rand, O. |
GROUND EFFECT MODELING FOR ROTARY-WING SIMULATION |
ICAS 2008-5.11.3 |
| Ranieri, A. |
CONTRACT-BASED AIR TRANSPORTATION SYSTEM TO FULFILL THE ARRIVING-ON-TIME OBJECTIVE |
ICAS 2008-8.2.1 |
| Rasuo, B. |
ON AIRCRAFT PERFORMANCE IMPROVEMENT BY USING WINGLETS |
ICAS 2008-2.8.3 |
| Rasuo, B. |
ON RESULTS’ ACCURACY AT TWO-DIMENSIONAL WIND TUNNEL TESTING |
ICAS2008-P2.12 |
| Rasuo, B. |
ON-CONDITION MAINTENANCE FOR NON-MODULAR JET ENGINES: AN EXPERIENCE |
ICAS 2008-4.5.2 |
| Rathinam, S. |
AN OPTIMIZATION MODEL FOR REDUCING AIRCRAFT TAXI TIMES AT THE DALLAS-FORT WORTH INTERNATIONAL AIRPORT |
ICAS 2008-8.6.1 |
| Rauen, A. |
EUROFIGHTER/TYPHOON PROGRAMME |
ICAS 2008-0.5 |
| Ravachol, M. |
UNCERTAINTIES AT THE CONCEPTUAL STAGE: MULTILEVEL MULTIDISCIPLINARY DESIGN AND OPTIMIZATION APPROACH |
ICAS 2008-1.1.2 |
| Rebentisch, E. |
LEAN PRODUCT DEVELOPMENT IN THE AEROSPACE ENTERPRISE |
ICAS 2008-6.7.1 |
| Reckzeh, D. |
AERODYNAMIC DESIGN OF THE A400M HIGH-LIFT SYSTEM |
ICAS 2008-2.7.2 INVITED |
| Reed, H. L. |
COMPUTATIONS FOR LAMINAR FLOW CONTROL IN SWEPT-WING BOUNDARY LAYERS |
ICAS 2008-2.7.4 |
| Reed, H. L. |
FLIGHT EXPERIMENTS ON SWEPT WING TRANSITION USING DISTRIBUTED ROUGHNESS |
ICAS 2008-2.7.5 |
| Régert, T. |
INVESTIGATION ON THE EFFECT OF HYDRODYNAMIC MEMS ON AIRFOIL |
ICAS2008-3.10 ST: |
| Rehman, A. |
FRAMEWORK OF PAKISTAN AEROSPACE INDUSTRY QUALITY SYSTEM |
ICAS 2008-6.9.4 |
| Reinartz, B. U. |
PERFORMANCE ANALYSIS OF A 3D SCRAMJET INTAKE |
ICAS 2008-4.1.1 |
| Reis, M. V. F. |
A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
| Renaud, G. |
STATIC AND FATIGUE ANALYSIS OF AN UPPER WING SKIN WITH EXFOLIATION CORROSION |
ICAS 2008-7.4.1 |
| Rendall, T. C. S. |
TOWARDS AERODYNAMIC OPTIMISATION OF AN AEROELASTIC WING USING DOMAIN ELEMENT PARAMETERISATION |
ICAS 2008-2.8.1 |
| Resende, H. B. |
EVOLUTION OF EMBRAER’S CIVIL AIRCRAFT |
ICAS 2008-1.7.1 INVITED |
| Reß, R. |
FIN BUFFET CHARACTERISTICS OF ADVANCED TRAINER AIRCRAFT |
ICAS 2008-3.4.1 |
| Reyer, M. |
A WALL SHEAR STRESS MEASUREMENT TECHNIQUE USING THE THERMAL WAKES OF SMALL HEATED SPOTS |
ICAS 2008-3.7.1 |
| Reynolds, N. D. |
MODELING OF ACOUSTICALLY TREATED NACELLE LIP TRANSPIRATION FLOW ANTI-ICING SYSTEM |
ICAS 2008-6.4.3 |
| Reynolds, T. G. |
ANALYSIS OF LATERAL FLIGHT INEFFICIENCY IN GLOBAL AIR TRAFFIC MANAGEMENT |
ICAS 2008-11.3.1 (AIAA 2008-8865) |
| Reynolds, T. G. |
NETWORK AND ENVIRONMENTAL IMPACTS OF PASSENGER AND AIRLINE RESPONSE TO COST AND DELAY |
ICAS 2008-10.4.4 (AIAA 2008-8890) |
| Rezaee, M. |
FEM MICRO-MECHANICAL ANALYSIS OF DELAMINATION PHENOMENON IN IMC LAMINATED COMPOSITES USING DAMAGE THEORY |
ICAS2008-9.4 ST: |
| Rhodes, J. |
RELATIONSHIP OF MAXIMUM MANAGEABLE AIR TRAFFIC CONTROL COMPLEXITY AND SECTOR CAPACITY |
ICAS 2008-8.2.3 |
| Rhodes, R. G. |
COMPUTATIONS FOR LAMINAR FLOW CONTROL IN SWEPT-WING BOUNDARY LAYERS |
ICAS 2008-2.7.4 |
| Riabov, V. V. |
HEAT TRANSFER ON HYPERSONIC BLUNT BODIES WITH GAS INJECTION |
ICAS 2008-3.6.4 |
| Riabov, V. V. |
NUMERICAL AND EXPERIMENTAL STUDIES OF SHOCK INTERFERENCE IN HYPERSONIC FLOWS NEAR A CYLINDER |
ICAS2008-P2.3 |
| Riccabone, A. |
METHODOLOGY OPTIMIZATION OF METAL CUTTING PROGRAMMING APPLIED TO AERONAUTICAL COMPONENTS |
ICAS 2008-6.10.5 |
| Ricci, S. |
DEVELOPMENT AND VALIDATION OF A NEXT-GENERATION CONCEPTUAL AERO-STRUCTURAL SIZING SUITE |
ICAS 2008-1.6.2 |
| Ricci, S. |
DEVELOPMENT AND VALIDATION OF AN INVESTIGATION TOOL FOR NONLINEAR AEROELASTIC ANALYSIS |
ICAS 2008-9.6.3 |
| Ricciardi, J. |
CESSNA CITATION CJ1 FLIGHT TEST DATA GATHERING AND LEVEL-C SIMULATOR MODEL DEVELOPMENT |
ICAS 2008-5.1.2 |
| Riccobene, L. |
DEVELOPMENT AND VALIDATION OF A NEXT-GENERATION CONCEPTUAL AERO-STRUCTURAL SIZING SUITE |
ICAS 2008-1.6.2 |
| Rieger, H. |
AERODYNAMIC OPTIMIZATION OF AIRCRAFT CONFIGURATIONS WITH MULTIDISZIPLINARY ASPECTS |
ICAS 2008-2.11.3 |
| Riggins, D. |
NUMERICAL STUDY OF ENERGY UTILIZATION IN NOZZLE/PLUME FLOW-FIELDS OF HIGH-SPEED AIR-BREATHING VEHICLES |
ICAS 2008-4.3.3 |
| Rihacek, C. |
CONTRACT-BASED AIR TRANSPORTATION SYSTEM TO FULFILL THE ARRIVING-ON-TIME OBJECTIVE |
ICAS 2008-8.2.1 |
| Rikards, R. |
METAMODELS FOR THE OPTIMIZATION OF DAMAGE-TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.3.3 |
| Rinoie, K. |
VORTEX BEHAVIORS OF CRANKED ARROW WING CONFIGURATIONS WITH DIFFERENT WING PLANFORMS |
ICAS 2008-3.3.2 |
| Rinoie, K. |
WING DESIGN OF SUPERSONIC TRANSPORT BY A MULTI-POINT OPTIMIZATION METHOD |
ICAS 2008-2.4.3 |
| Rios, J. |
SOLVING HIGH-FIDELITY, LARGE-SCALE TRAFFIC FLOW MANAGEMENT PROBLEMS IN REDUCED TIME |
ICAS 2008-11.7.4 (AIAA 2008-8910) |
| Rispoli, A. |
DEVELOPMENT AND TEST OF AN INTEGRATED SENSOR SYSTEM FOR AUTONOMOUS COLLISION AVOIDANCE |
ICAS2008-P6.12 |
| Rix, O. |
INNOVATIVE APPROACH FOR FUTURE AIRCRAFT DEVELOPMENT AT IAI |
ICAS 2008-1.6.1 |
| Rizzi, A. |
CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
| Robinson, R. |
SECURITY ARCHITECTURE AND FORMAL ANALYSIS OF AN AIRPLANE SOFTWARE DISTRIBUTION SYSTEM |
ICAS 2008-9.1.1 |
| Robinson, R. |
SECURITY OF WIRELESS SENSOR NETWORK ENABLED HEALTH MONITORING FOR FUTURE AIRPLANES |
ICAS 2008-9.1.3 |
| Robinson, R. V. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
| Rocha, B. |
ON THE DEVELOPMENT OF METHODS AND TECHNIQUES FOR AIRCRAFT STRUCTURAL HEALTH MONITORING |
ICAS2008-7.4 ST: |
| Roget, B. |
PREDICTION OF HELICOPTER MANEUVER LOADS USING A TIGHTLY COUPLED CFD/CSD ANALYSIS |
ICAS 2008-2.10.4 |
| Rohács, J. |
FEASIBILITY STUDY ON MULTI-PHASE FLOW SIMULATION OF FUEL INJECTION USING LATTICE BOLTZMANN METHOD |
ICAS 2008-4.3.4 |
| Rohács, J. |
INVESTIGATION ON THE EFFECT OF HYDRODYNAMIC MEMS ON AIRFOIL |
ICAS2008-3.10 ST: |
| Roling, P. C. |
EVALUATION OF ANCHORAGE INTERNATIONAL AIRPORT USING THE AIRPORT BUSINESS SUITE |
ICAS 2008-10.4.5 (AIAA 2008-8891) |
| Roof, C. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
| Rosa Taddei, S. |
EULER INVERSE THROUGHFLOW MODEL BASED ON AN IMPLICIT UPWIND TIME MARCHING TECHNIQUE |
ICAS 2008-2.3.2 |
| Rosenberger, J. |
QUEUEING NETWORK MODELS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.10.3 (AIAA 2008-8942) |
| Ross, H. |
FLY AROUND THE WORLD WITH A SOLAR POWERED AIRPLANE |
ICAS 2008-10.11.1 (AIAA 2008-8954 ) |
| Ross, K. |
SOLVING HIGH-FIDELITY, LARGE-SCALE TRAFFIC FLOW MANAGEMENT PROBLEMS IN REDUCED TIME |
ICAS 2008-11.7.4 (AIAA 2008-8910) |
| Rouwhorst, W. F. J. A. |
PILOTED SIMULATION RESULTS OF AN ONBOARD WAKE VORTEX DETECTION, WARNING AND AVOIDANCE SYSTEM AND COCKPIT DISPLAY ASPECTS |
ICAS 2008-9.9.1 |
| Rowe, D. |
AIRSPACE SECURITY MEASURES EMPLOYED FOR THE UN GENERAL ASSEMBLY MEETING: ANALYSIS AND IMPACT |
ICAS 2008-11.5.1 (AIAA 2008-8892) |
| Rozen, N. |
AN AUTOMATED SIMULATION PILOT CAPABILITY TO SUPPORT ADVANCED AIR TRAFFIC CONTROLLER TRAINING |
ICAS 2008-10.5.3 (AIAA 2008-8897) |
| Rudolph, I. |
A WALL SHEAR STRESS MEASUREMENT TECHNIQUE USING THE THERMAL WAKES OF SMALL HEATED SPOTS |
ICAS 2008-3.7.1 |
| Rudolph, M. |
AUGMENTED VISION VIDEOPANORAMA SYSTEM FOR REMOTE AIRPORT TOWER OPERATION |
ICAS 2008-8.3.1 |
| Ruijgrok, G. J. J. |
ON THE REDUCTION OF NOX-EMISSION LEVELS BY PERFORMING LOW NOX FLIGHTS |
ICAS2008-4.7 ST: |
| Rumizen, M. |
THE FEASIBILITY AND POTENTIAL ENVIRONMENTAL BENEFITS OF ALTERNATIVE FUELS FOR COMMERCIAL AVIATION |
ICAS 2008-4.7.5 |
| Ruzzene, M. |
DESIGN AND MANUFACTURING OF COMPOSITE CHIRAL STRUCTURES WITH MORPHING CAPABILITIES |
ICAS 2008-7.8.1 |
| S., Shinji |
643 DEVELOPMENT OF A COAXIAL ROTOR MAV FOR INDOOR APPLICATION |
ICAS2008-P1.9 |
| Saarela, O. |
COMPRESSION STRENGTH OF NOTCHED AND IMPACT DAMAGED COMPOSITE LAMINATES |
ICAS 2008-7.5.2 |
| Sachs, G. |
IMPROVEMENT FOR LANDING ON SMALL-MEDIUM AIRPORTS USING FUTURE, AIRCRAFT-AUTONOMOUS GUIDANCE AIDS |
ICAS 2008-5.7.1 INVITED |
| Sachs, G. |
TRAJECTORY CONTROL IMPROVEMENT BASED ON A NONLINEAR DYNAMIC INVERSION APPROACH |
ICAS 2008-5.7.2 |
| Sachs, G. |
UNIQUE PERFORMANCE CHARACTERISTICS OF SOLAR AIRCRAFT |
ICAS 2008-5.3.2 |
| Sachs, H. |
MONITORING OF OSCILLATORY FAILURE CASES FOR THE REDUCTION OF STRUCTURAL LOADS IN AN AEROELASTIC AIRCRAFT |
ICAS 2008-7.7.2 |
| Sadraey, M. |
A SYSTEMATIC APPROACH IN AIRCRAFT CONFIGURATION DESIGN OPTIMIZATION |
ICAS 2008-1.9.1 (AIAA 2008-8926) |
| Safarik, P. |
SEPARATION CONTROL BY SYNTHETIC JET ACTUATOR IN STRAIGHT BLADE CASCADE |
ICAS 2008-3.10.4 |
| Saggiani, G. M. |
FLIGHT MECHANICS SIMULATOR FOR ROTORCRAFT DEVELOPMENT |
ICAS2008-P5.4 |
| Sainadh, A. |
INCLUSION OF ENGINE RELATED PARAMETERS IN CONCEPTUAL DESIGN OF MORPHING AIRCRAFT |
ICAS 2008-1.6.4 |
| Saint-Martin, P. de |
DESIGN OF A SMALL SUPERSONIC TRANSPORT AIRCRAFT WITH HIGH ENVIRONMENTAL CONSTRAINTS |
ICAS 2008-1.10.1 INVITED |
| Sala, G. |
DESIGN AND MANUFACTURING OF COMPOSITE CHIRAL STRUCTURES WITH MORPHING CAPABILITIES |
ICAS 2008-7.8.1 |
| Samardzic, M. |
APPLICATION OF SEMICONDUCTOR STRAIN GAUGES IN MEASUREMENTS OF DYNAMIC STABILITY DERIVATIVES IN THE T-38 WIND TUNNEL |
ICAS 2008-3.4.5 |
| Samardzic, M. |
PROTOTYPE OF A STIFF WIND TUNNEL BALANCE WITH SEMICONDUCTOR STRAIN GAUGES AND THERMOCOMPENSATION DONE BY SOFTWARE |
ICAS2008-P2.9 |
| Sammut, A. |
DESIGN OF EXPERIMENT FOR THE PILOT EVALUATION OF AN AIRBORNE RUNWAY INCURSION ALERTING SYSTEM |
ICAS 2008-9.10.2 |
| Sampigethaya, K. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
| Sampigethaya, K. |
SECURITY OF WIRELESS SENSOR NETWORK ENABLED HEALTH MONITORING FOR FUTURE AIRPLANES |
ICAS 2008-9.1.3 |
| Samuelsson, L. |
FATIGUE ANALYSIS: THE SUPER-NEUBER TECHNIQUE FOR CORRECTION OF LINEAR ELASTIC FE RESULTS |
ICAS 2008-7.4.2 |
| Sant, R. |
AERODYNAMIC OPTIMIZATION OF A BLENDED WING BODY |
ICAS2008-2.11 ST: |
| Santema, S. C. |
DESIGN OF A LEAN MRO BUSINESS PROCESS FOR EPCOR |
ICAS 2008-10.3.4 (AIAA 2008-8864) |
| Santos, L. C. C. |
A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
| Saric, W. S. |
COMPUTATIONS FOR LAMINAR FLOW CONTROL IN SWEPT-WING BOUNDARY LAYERS |
ICAS 2008-2.7.4 |
| Saric, W. S. |
FLIGHT EXPERIMENTS ON SWEPT WING TRANSITION USING DISTRIBUTED ROUGHNESS |
ICAS 2008-2.7.5 |
| Sarma, A. |
AIRSHIP TRANSPORT OPERATIONAL MANAGEMENT IN NORTHERN LATITUDES |
ICAS 2008-10.1.1 (AIAA 2008-8850) |
| Sarma, A. |
AN ATMOSPHERIC SIMULATION SYSTEM FOR AVIATION REQUIREMENTS OVER NORTHERN LATITUDES |
ICAS 2008-10.7.2 (AIAA 2008-8915) |
| Sato, H. |
OPTIMUM AEROELASTIC DESIGN OF A RESONANCE TYPE FLAPPING WING FOR MICRO AIR VEHICLES |
ICAS 2008-7.10.3 |
| Sato, K. |
LOW-BOOM AND LOW-DRAG OPTIMIZATION FOR THE TWIN-ENGINE SILENT SUPERSONIC TECHNOLOGY DEMONSTRATOR |
ICAS 2008-2.4.1 |
| Scarano, F. |
INVESTIGATION OF THE FLOW IN A RECTANGULAR CAVITY USING TOMOGRAPHIC AND TIME-RESOLVED PIV |
ICAS 2008-3.2.2 |
| Schafer, A. |
MODELLING AIRLINE ROUTING AND SCHEDULING UNDER AIRPORT CAPACITY CONSTRAINTS |
ICAS 2008-11.1.2 (AIAA 2008-8855) |
| Schäfer, A. |
NETWORK AND ENVIRONMENTAL IMPACTS OF PASSENGER AND AIRLINE RESPONSE TO COST AND DELAY |
ICAS 2008-10.4.4 (AIAA 2008-8890) |
| Schaller, J. |
IMPROVEMENT FOR LANDING ON SMALL-MEDIUM AIRPORTS USING FUTURE, AIRCRAFT-AUTONOMOUS GUIDANCE AIDS |
ICAS 2008-5.7.1 INVITED |
| Schaller, J. |
92 LANDING-AVIONIC SYSTEM FOR SMALL-MEDIUM AIRCRAFT FOR AUTOMATED LANDING ON SMALL-MEDIUM AND/OR POORLY EQUIPPED AIRPORTS |
ICAS2008-P6.8 |
| Scharl, J. |
ANALYSIS OF ARRIVAL MANAGEMENT PERFORMANCE WITH AIRCRAFT REQUIRED TIME OF ARRIVAL CAPABILITIES |
ICAS 2008-11.9.3 (AIAA 2008-8932) |
| Schauenburg, A. |
FLEET MANAGEMENT SYSTEM FOR AN ADVANCED HELICOPTER PLATFORM - DESIGN & DEVELOPMENT REQUIREMENTS |
ICAS 2008-6.11.1 |
| Schaufele, R. |
IMPACT OF US-EU OPEN AREA AVIATION TREATY ON US AVIATION: A PARAMETRIC ANALYSIS WITH SIMULATION |
ICAS 2008-10.10.3 (AIAA 2008-8937) |
| Scherillo, F. |
SINGLE VERSUS MULTIPLE WINGLETS: NUMERICAL AND EXPERIMENTAL INVESTIGATION |
ICAS 2008-2.7.3 |
| Schmid, A. |
FIN BUFFET CHARACTERISTICS OF ADVANCED TRAINER AIRCRAFT |
ICAS 2008-3.4.1 |
| Schmidt, M. |
AUGMENTED VISION VIDEOPANORAMA SYSTEM FOR REMOTE AIRPORT TOWER OPERATION |
ICAS 2008-8.3.1 |
| Schmidt, R. C. |
APPLICATION OF THE INTEGRATED PRODUCT TEAM (IPT) CONCEPT TO THE RE-ENGINE OF A VERY LIGHT JET (VLJ) |
ICAS 2008-6.7.5 |
| Schmitt, D -R. |
REAL TIME SIMULATION OF INTEGRATION OF UAV'S INTO AIRSPACE |
ICAS 2008-8.1.1 |
| Schoemig, E. |
ANALYSIS OF ARRIVAL MANAGEMENT PERFORMANCE WITH AIRCRAFT REQUIRED TIME OF ARRIVAL CAPABILITIES |
ICAS 2008-11.9.3 (AIAA 2008-8932) |
| Scholz, D. |
THE GREEN FREIGHTER PROJECT - OBJECTIVES AND FIRST RESULTS |
ICAS 2008-4.10.3 |
| Schönfeld, T. |
THE REGIONAL AEROSPACE CLUSTER POLICY IN EUROPE |
ICAS 2008-6.9.2 |
| Schreiber, R. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
| Schroijen, M. J. T. |
PROPELLER SLIPSTREAM INVESTIGATION USING THE FOKKER F27 WIND TUNNEL MODEL WITH FLAPS DEFLECTED |
ICAS 2008-3.1.2 |
| Schuck, F. |
IMPROVEMENT FOR LANDING ON SMALL-MEDIUM AIRPORTS USING FUTURE, AIRCRAFT-AUTONOMOUS GUIDANCE AIDS |
ICAS 2008-5.7.1 INVITED |
| Schuster, W. |
SATELLITE-BASED NAVIGATION ARCHITECTURE STUDY FOR AIRCRAFT CATEGORY III LANDINGS |
ICAS 2008-6.4.4 |
| Schut, E. J. |
DEVELOPMENT AND IMPLEMENTATION OF KNOWLEDGE-BASED DESIGN PROCESS PRIMITIVES |
ICAS 2008-6.10.4 |
| Schwartz, A. |
RELATIONSHIP OF MAXIMUM MANAGEABLE AIR TRAFFIC CONTROL COMPLEXITY AND SECTOR CAPACITY |
ICAS 2008-8.2.3 |
| Schwarz, C. |
AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION FOR TAKE-OFF AND DEPARTURE |
ICAS 2008-11.8.3 (AIAA 2008-8921) |
| Schwarz, C. |
ALLEVIATION OF ATMOSPHERIC FLOW DISTURBANCE EFFECTS ON AIRCRAFT RESPONSE |
ICAS 2008-5.2.2 |
| Schwerin, D. |
DESIGN FOR PROCESS EXCELLENCE - ENSURING TIMELY AND COST EFFECTIVE SOLUTIONS |
ICAS 2008-6.7.4 |
| Scott, M. L. |
LOADED CARBON COMPOSITE SCARF JOINTS SUBJECT TO QUASI STEADY LATERAL LOADS |
ICAS 2008-7.2.2 |
| Seeckt, K. |
THE GREEN FREIGHTER PROJECT - OBJECTIVES AND FIRST RESULTS |
ICAS 2008-4.10.3 |
| Segall, D. |
FLIGHT EVALUATION OF A COMPACT AIRBORNE TRACE GAS ANALYSIS SENSOR PROOF-OF-CONCEPT |
ICAS2008-P6.4 |
| Seifert, J. |
A NEW APPROACH FOR CO2 REDUCTION APPLYING STATE-OF-THE-ART ENGINE AND AIRFRAME TECHNOLOGY |
ICAS2008-4.2 ST (AIAA 2008-8974) |
| Seifert, J. |
POTENTIALS OF LIGHTER-THAN-AIR TECHNOLOGY IN FUTURE MARKETS – AN EVALUATION |
ICAS2008-P1.7 |
| Seifert, J. |
PROMISING FUTURE AIRCRAFT CONCEPT – ESTOL |
ICAS2008-P1.8 |
| Seitz, A. |
A NEW APPROACH FOR CO2 REDUCTION APPLYING STATE-OF-THE-ART ENGINE AND AIRFRAME TECHNOLOGY |
ICAS2008-4.2 ST (AIAA 2008-8974) |
| Selier, M. |
NATIONAL TECHNOLOGY PROJECT 'OUTCAST' ON UAV SENSE AND AVOID |
ICAS 2008-8.1.2 |
| Sénési, S. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
| Sengstacken, A. |
UTILIZATION OF NETWORK THEORY FOR THE ENHANCEMENT OF ATO AIR ROUTE FORECAST |
ICAS 2008-11.10.5 (AIAA 2008-8944) |
| Sengupta, P. |
QUEUEING NETWORK MODELS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.10.3 (AIAA 2008-8942) |
| Serena Guinzio, P. |
A DUAL-DUPLEX ELECTROHYDRAULIC SYSTEM FOR THE FLY-BY-WIRE CONTROL OF A HELICOPTER MAIN ROTOR |
ICAS 2008-6.6.4 |
| Seuschek, H. |
MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
| Shah, S. |
PREDICTION OF DELAMINATION IN ADVANCED AEROSPACE COMPOSITE STRUCTURES USING MICRO/MACRO MECHANICS CONSTITUTIVE METHODS |
ICAS 2008-7.5.3 |
| Shao, L. M. |
EXPERIMENTAL RESEARCH OF FLAPPING-WING PROPULSION FOR MICRO AIR VEHICLES |
ICAS2008-3.4 ST: |
| Shao, P. C. |
IDENTIFYING FATIGUE OF FLIGHT ATTENDANTS IN SHORT-HAUL OPERATIONS |
ICAS 2008-9.2.3 |
| Sharma, T. |
ADVANCED METHODOLOGIES FOR AVERAGE PROBABILITY CALCULATION FOR AEROSPACE SYSTEMS |
ICAS 2008-9.3.3 |
| Sheth, K. S. |
TASK ANALYSIS FOR FEASIBILITY ASSESSMENT OF A COLLABORATIVE TRAFFIC FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.7.3 (AIAA 2008-8909) |
| Shetty, S. |
SYSTEM OF SYSTEMS DESIGN FOR WORLDWIDE COMMERCIAL AIRCRAFT NETWORKS |
ICAS 2008-8.4.1 |
| Shi, J. |
NEW METHOD TO ENHANCE THE WEARABILITY OF TITANIUM ALLOY ROTOR BLADE FOR AERO-ENGINE |
ICAS 2008-4.2.4 |
| Shin, H. S. |
INTEGRATED INTERCEPT MISSILE GUIDANCE AND CONTROL WITH TERMINAL ANGLE CONSTRAINT |
ICAS 2008-5.7.3 |
| Shin, H. S. |
NONLINEAR FORMATION GUIDANCE LAW WITH ROBUST DISTURBANCE OBSERVER |
ICAS 2008-5.7.4 |
| Shmilovich, A. |
FLOW CONTROL TECHNIQUES FOR TRANSPORT AIRCRAFT |
ICAS 2008-3.11.1 |
| Shoji, H. |
IMPACT CHARACTERISTICS ESTIMATION OF SHORT SUPPORT COLUMNS UNDER CABIN FLOOR |
ICAS 2008-9.4.1 |
| Sibilski, K. |
FLIGHT SAFETY AS CONSIDERED IN PROBABILISTIC TERMS |
ICAS 2008-9.3.4 |
| Sibilski, K. |
MODELING AND SIMULATION OF FLAPPING WINGS MICRO-AERIAL VEHICLES FLIGHT DYNAMICS |
ICAS 2008-5.9.1 INVITED |
| Sibilski, K. |
THE INFLUENCE OF FREE - PLAY AND FRICTION IN CONTROL SYSTEM ON AIRCRAFT DYNAMICS |
ICAS 2008-5.10.5 |
| Sieber, J. |
"ACTIVE CORE" - A KEY TECHNOLOGY FOR MORE ENVIRONMENTALLY FRIENDLY AERO ENGINES BEING INVESTIGATED UNDER THE NEWAC PROGRAM |
ICAS 2008-4.2.1 |
| Sijtsma, P. |
A NOVEL RECIPROCAL SOUND TRANSMISSION MEASURING METHOD, APPLIED ON A COMPOSITE FUSELAGE |
ICAS 2008-4.9.3 |
| Siladic, M. F. |
ON-CONDITION MAINTENANCE FOR NON-MODULAR JET ENGINES: AN EXPERIENCE |
ICAS 2008-4.5.2 |
| Silva Filho, D. H. |
EVOLUTION OF EMBRAER’S CIVIL AIRCRAFT |
ICAS 2008-1.7.1 INVITED |
| Silva, A. L. da |
A PROCEDURE TO DESIGN AIRCRAFT FLIGHT CONTROL LAWS TAKING INTO ACCOUNT ROBUSTNESS USING THE VARIABLE STRUCTURE CONTROL |
ICAS2008-5.4 ST: |
| Silva, R. F. A. F. |
A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
| Simeonides, G. A. |
LAMINAR-TURBULENT TRANSITION CORRELATION IN SUPERSONIC/ HYPERSONIC FLOW – ATTACHED VERSUS SEPARATED FLOW |
ICAS 2008-3.8.3 |
| Singh, C. |
AERODYNAMIC STALL SUPPRESSION ON AEROFOIL SECTIONS USING PASSIVE AIR JET VORTEX GENERATORS |
ICAS 2008-3.11.3 |
| Sinha, A. |
DESIGN OF A NOVEL INTELLIGENT DATA MANAGEMENT TOOL FOR HEALTH AND USAGE MONITORING SYSTEMS – DESIGN REQUIREMENTS |
ICAS2008-6.1 ST: |
| Sinha, A. K. |
EVALUATION OF AN INTEROPERABLE VERTICAL TAKE-OFF UAV FOR OPERATIONS WITH UGVS - AN OVERVIEW |
ICAS 2008-6.11.2 |
| Sinha, A. K. |
FLEET MANAGEMENT SYSTEM FOR AN ADVANCED HELICOPTER PLATFORM - DESIGN & DEVELOPMENT REQUIREMENTS |
ICAS 2008-6.11.1 |
| Sitaraman, J. |
PREDICTION OF HELICOPTER MANEUVER LOADS USING A TIGHTLY COUPLED CFD/CSD ANALYSIS |
ICAS 2008-2.10.4 |
| Slingerland, R. |
PROPELLER SLIPSTREAM INVESTIGATION USING THE FOKKER F27 WIND TUNNEL MODEL WITH FLAPS DEFLECTED |
ICAS 2008-3.1.2 |
| Smaili, M. H. |
A SIMULATION BENCHMARK FOR AIRCRAFT SURVIVABILITY ASSESSMENT |
ICAS 2008-9.3.2 |
| Smaili, M. H. |
OPTIMISING HIGH-EFFICIENCY RUDDERS FOR TRANSPORT AIRCRAFT FUEL BURN REDUCTION |
ICAS 2008-2.11.2 |
| Smid, R. |
EMAT APPLIED IN THE AVIATION INDUSTRY |
ICAS2008-P1.1 (AIAA 2008-8870) |
| Smith, A. |
AN ADAPTABLE METHODOLOGY FOR AUTOMATION APPLICATION DEVELOPMENT |
ICAS 2008-6.2.3 |
| Smith, A. P. |
SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
| Smith, B. E. |
A PROGNOSTIC METHOD TO IDENTIFY HAZARDS FOR FUTURE AVIATION CONCEPTS |
ICAS 2008-9.3.1 |
| Smith, E. |
OPERATIONAL ACCEPTABILITY OF ISSUING RNAV/RNP PROCEDURE CHANGES IN FUTURE TERMINAL ENVIRONMENTS |
ICAS2008-11.8 ST (AIAA 2008-8922) |
| Smith, H. |
NOVEL DESIGN CONCEPTS FOR AIRCRAFT WITH REDUCED NOISE AND GLOBAL WARMING CHARACTERISTICS |
ICAS 2008-4.10.4 |
| Smith, J. C. |
A PERFORMANCE ASSESSMENT OF A TACTICAL AIRBORNE SEPARATION ASSISTANCE SYSTEM USING REALISTIC, COMPLEX TRAFFIC FLOWS |
ICAS 2008-11.4.4 (AIAA 2008-8884) |
| Smith, N. |
CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
| Smrcek, L. |
PERFORMANCE DEGRADATION OF A SIMULATED ICE CONTAMINATED AIRFOIL BY SUPER-COOLED DROPLETS |
ICAS 2008-3.7.2 |
| Sobester, A. |
THE QUEST FOR A TRULY PARSIMONIOUS AIRFOIL PARAMETERIZATION SCHEME |
ICAS2008-P2.2 (AIAA 2008-8879) |
| Soedarsono, A. A. |
DEVELOPMENT OF UNMANNED AERIAL VEHICLE IN BPPT |
ICAS2008-P1.10 |
| Sohn, M. |
DELTA-WING VORTEX CONTROL BY APEX STRAKE AND MICRO LEADING-EDGE FLAP |
ICAS2008-3.3 ST: |
| Sollo, A. |
FE STUDY OF WINDSHIELD SUBJECTED TO HIGH SPEED BIRD IMPACT |
ICAS 2008-9.4.3 |
| Solomos, G. |
AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
| Somos, M. |
PARAMETER IDENTIFICATION OF FLYING WING WITH SIGNIFICANT DEFORMATION |
ICAS 2008-5.8.1 |
| Song, B. |
DEVELOPMENT OF FLAPPING WING MICRO AIR VEHICLE |
ICAS 2008-1.5.3 |
| Song, B. F. |
COORDINATELY MODELING AND SIMULATION OF THE EJECTION SEAT/OCCUPANT SYSTEM |
ICAS2008-P9.3 |
| Song, B. F. |
ERGONOMIC ASSESSMENT METHOD FOR COCKPIT LAYOUT OF CIVIL AIRCRAFT X BASED ON VIRTUAL DESIGN |
ICAS2008-P6.5 |
| Song, B. F. |
EXPERIMENTAL RESEARCH OF FLAPPING-WING PROPULSION FOR MICRO AIR VEHICLES |
ICAS2008-3.4 ST: |
| Song, B. F. |
HEALTH MONITORING FOR AEROCRAFT STRUCTURE SYSTEM BY HARMONIC WAVELET TRANSFORM |
ICAS2008-7.7 ST: |
| Song, B. F. |
LOW REYNOLDS NUMBER TANDEM OR DIAMOND WING UAV AERODYNAMICS CENTER RESEARCH BASED ON RESPONSE SURFACE METHOD |
ICAS2008-3.1 ST: |
| Song, B. F. |
METHODS FOR CALCULATING THE DAMAGE-RATE OF AIRCRAFT COMPONENT |
ICAS2008-9.8 ST: |
| Song, B. F. |
NUMERICAL SIMULATION OF 3D FLAPPING WING BASED ON CHIMERA METHOD |
ICAS 2008-2.10.5 |
| Song, B. F. |
THE SIMULATION OF THE HUMAN-MACHINE PARTNERSHIP IN UCAV OPERATION |
ICAS 2008-9.10.5 |
| Song, K. |
LIFT PREDICTION OF MULTI-ELEMENT AIRFOIL USING DES AND RANS |
ICAS2008-P2.5 |
| Song, L. |
METHODOLOGIES FOR ESTIMATING THE IMPACT OF SEVERE WEATHER ON AIRSPACE CAPACITY |
ICAS 2008-10.7.4 (AIAA 2008-8917) |
| Song, W. P. |
NUMERICAL SIMULATION OF 3D FLAPPING WING BASED ON CHIMERA METHOD |
ICAS 2008-2.10.5 |
| Soper, T. J. |
DRAG AND FLOW REGIMES ASSOCIATED WITH RECTANGULAR CAVITIES AT YAW AT LOW SPEEDS |
ICAS2008-P2.13 |
| Sorensen, K. |
AERODYNAMIC OPTIMIZATION OF AIRCRAFT CONFIGURATIONS WITH MULTIDISZIPLINARY ASPECTS |
ICAS 2008-2.11.3 |
| Sorli, M. |
A DUAL-DUPLEX ELECTROHYDRAULIC SYSTEM FOR THE FLY-BY-WIRE CONTROL OF A HELICOPTER MAIN ROTOR |
ICAS 2008-6.6.4 |
| Spadoni, A. |
DESIGN AND MANUFACTURING OF COMPOSITE CHIRAL STRUCTURES WITH MORPHING CAPABILITIES |
ICAS 2008-7.8.1 |
| Spano, E. |
EULER INVERSE THROUGHFLOW MODEL BASED ON AN IMPLICIT UPWIND TIME MARCHING TECHNIQUE |
ICAS 2008-2.3.2 |
| Speciale, G. |
TRAJECTORY OPTIMISATION FOR AUTONOMOUS VEHICLES: A MINIUAV APPLICATION |
ICAS 2008-5.6.3 |
| Speidel, J. |
INNOVATIVE FUTURE AIR TRANSPORT SYSTEM: SIMULATION OF A FULLY AUTOMATED ATS |
ICAS 2008-8.4.5 |
| Spence, G. T. |
REAL-TIME SIMULATION OF A DISTRIBUTED CONFLICT RESOLUTION ALGORITHM |
ICAS 2008-8.7.3 |
| Spies, G. |
OPERATIONAL CONCEPT FOR AN AIRPORT OPERATIONS CENTER TO ENABLE TOTAL AIRPORT MANAGEMENT |
ICAS 2008-8.3.2 |
| Spiker, M. A. |
REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
| Spogis, N. |
A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
| Sproewitz, T. |
THERMAL ASPECTS FOR COMPOSITE STRUCTURES - FROM MANUFACTURING TO IN-SERVICE PREDICTIONS |
ICAS 2008-7.9.4 |
| Sprong, K. P. |
IMPROVING TERMINAL OPERATIONS - BENEFITS OF RNAV DEPARTURE PROCEDURES AT DALLAS-FORT WORTH AND HARTSFIELD-JACKSON ATLANTA INTERNATIONAL AIRPORTS |
ICAS 2008-11.1.3 (AIAA 2008-8856) |
| Sridar, B. |
ESTIMATION OF AIR TRAFFIC DELAY USING THREE DIMENSIONAL WEATHER INFORMATION |
ICAS 2008-10.7.3 (AIAA 2008-8916) |
| Sridhar, B. |
PREDICTION OF WEATHER-RELATED DELAYS IN THE CONTINENTAL UNITED STATES |
ICAS 2008-8.2.2 |
| Srinivasan, R. |
FLIGHT EVALUATION OF A COMPACT AIRBORNE TRACE GAS ANALYSIS SENSOR PROOF-OF-CONCEPT |
ICAS2008-P6.4 |
| Stalnaker, S. |
INTEGRATED TIME-BASED FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.10.1 (AIAA 2008-8940) |
| Stamm, R. |
NETWORK ENABLED OPERATIONS ENHANCES AVIATION EFFICIENCY |
ICAS 2008-8.8.1 (AIAA 2008-8951) |
| Stanek, M. |
IHAAA STORE SEPARATION FROM CAVITY (SSC) PROJECT |
ICAS 2008-2.6.2 |
| Stapleton, S. |
INTEGRATED TIME-BASED FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.10.1 (AIAA 2008-8940) |
| Starik, A. |
INNOVATIONS IN COMBUSTION TECHNOLOGY FOR PROPULSION |
ICAS 2008-0.6 |
| Stassen, H. P. |
SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
| Stefanik, M. |
CAPACITY RESEARCH OF BRNO-TURANY AIRPORT WITH RESPECT TO NEW TRENDS IN AIR TRANSPORT |
ICAS 2008-8.5.3 |
| Steigenberge, J. |
MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
| Steinkellner, S. |
HOSTED SIMULATION FOR HETEROGENEOUS AIRCRAFT SYSTEM DEVELOPMENT |
ICAS2008-6.2 ST: |
| Stoica, A.-M. |
AUTOMATIC FLIGHT CONTROL USING SAMPLED-DATA MIXED H_2/H_INFINITY OPTIMISATION |
ICAS 2008-5.2.1 |
| Stoufflet, B |
DESIGN OF A SMALL SUPERSONIC TRANSPORT AIRCRAFT WITH HIGH ENVIRONMENTAL CONSTRAINTS |
ICAS 2008-1.10.1 INVITED |
| Streit, T. |
ACTIVE AND PASSIVE STRUCTURAL MEASURES FOR AEROELASTIC WINGLET DESIGN |
ICAS 2008-7.10.1 |
| Stroosma, O. |
A SIMULATION BENCHMARK FOR AIRCRAFT SURVIVABILITY ASSESSMENT |
ICAS 2008-9.3.2 |
| Strybel, T. Z. |
COMPARING SITUATION AWARENESS MEASUREMENT TECHNIQUES IN A LOW FIDELITY AIR TRAFFIC CONTROL SIMULATION |
ICAS 2008-9.7.4 |
| Stuip, M. |
NATIONAL TECHNOLOGY PROJECT 'OUTCAST' ON UAV SENSE AND AVOID |
ICAS 2008-8.1.2 |
| Stumpf, E. |
A HOLISTIC APPROACH TO EVALUATE THE AIR TRANSPORTATION SYSTEM |
ICAS 2008-8.4.2 |
| Styuart, A. V. |
PROBABILISTIC MODELING OF STRUCTURAL / AEROELASTIC LIFE CYCLE FOR RELIABILITY EVALUATION OF DAMAGE TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.1.1 |
| Su, J. M. |
LOW REYNOLDS NUMBER TANDEM OR DIAMOND WING UAV AERODYNAMICS CENTER RESEARCH BASED ON RESPONSE SURFACE METHOD |
ICAS2008-3.1 ST: |
| Su, R. E. |
ERGONOMIC ASSESSMENT METHOD FOR COCKPIT LAYOUT OF CIVIL AIRCRAFT X BASED ON VIRTUAL DESIGN |
ICAS2008-P6.5 |
| Subbarao, K. |
QUEUEING NETWORK MODELS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.10.3 (AIAA 2008-8942) |
| Subbarao, K. |
TRAJECTORY UNCERTAINTY MODELING FOR QUEUEING ANALYSIS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.1.1 (AIAA 2008-8854) |
| Suikat, R. |
OPERATIONAL CONCEPT FOR AN AIRPORT OPERATIONS CENTER TO ENABLE TOTAL AIRPORT MANAGEMENT |
ICAS 2008-8.3.2 |
| Sulaeman, E. |
646 ANALYTICAL FORMULATION FOR NON-UNIFORM BEAM FINITE ELEMENT |
ICAS2008-P3.10 |
| Suleman, A. |
ON THE DEVELOPMENT OF METHODS AND TECHNIQUES FOR AIRCRAFT STRUCTURAL HEALTH MONITORING |
ICAS2008-7.4 ST: |
| Sumi, T. |
HIGH-ORDER LARGE EDDY SIMULATION AROUND 2-D AEROFOIL WITH HIGH-LIFT DEVICE |
ICAS 2008-2.1.2 |
| Sumi, T. |
INTERFACE CONDITIONS OF FINITE-DIFFERENCE COMPACT SCHEMES FOR COMPUTATIONAL AEROACOUSTICS |
ICAS 2008-2.3.1 |
| Sumi, T. |
LARGE EDDY SIMULATION AROUND 2-D AIRFOIL WITH NATURAL TRANSITION AT HIGH REYNOLDS NUMBERS |
ICAS2008-2.1 ST: |
| Sun, C. |
OPTIMIZATION DESIGN ON PLATE-RIB STRUCTURE FOR CERTAIN KINDS OF AIRCRAFT |
ICAS 2008-9.5.3 |
| Sun, D. C. |
CFD RESEARCH FOR AIR-TO-AIR MISSILE WITH LATERAL JET CONTROL |
ICAS2008-2.64 ST: |
| Sun, L. |
ADAPTING THE ACCIMAP FOR AN ANALYSIS OF THE SQ006 ACCIDENT |
ICAS2008-P9.1 (AIAA 2008-8878) |
| Sun, Q. |
STUDY ON THE RELATIONSHIP BETWEEN CORROSION DAMAGE AND RESIDUAL STRENGTH OF AL 7075-T6 ALLOY |
ICAS 2008-9.8.2 |
| Sun, W. |
PROMISING FUTURE AIRCRAFT CONCEPT – ESTOL |
ICAS2008-P1.8 |
| Sun, Y. F. |
THE SYSTEM FAULT BEHAVIOR AND MODEL |
ICAS2008-P9.2 |
| Sun, Y. J. |
THE APPLICATION OF THE MORLET WAVELET ON RESPONSE FILTERING OF THE HELICOPTER CANNON’S RECOIL |
ICAS2008-P3.5 |
| Sunderlin, J. |
OPERATIONAL ASSESSMENT OF THE INTEGRATED TERMINAL WEATHER SYSTEM (ITWS) USING DIRECT MEASUREMENT |
ICAS 2008-10.7.5 (AIAA 2008-8918) |
| Surace, C. |
A NEGATIVE SELECTION APPROACH TO DETECT DAMAGE IN AERONAUTICAL STRUCTURES WITH CHANGING OPERATING CONDITIONS |
ICAS 2008-9.4.2 |
| Surace, G. |
A NEGATIVE SELECTION APPROACH TO DETECT DAMAGE IN AERONAUTICAL STRUCTURES WITH CHANGING OPERATING CONDITIONS |
ICAS 2008-9.4.2 |
| Sutherland, A. N. |
A SMALL SCALE PITCH-PLUNGE FLUTTER MODEL FOR ACTIVE FLUTTER CONTROL RESEARCH |
ICAS 2008-3.4.4 |
| Suzuki, H. |
TRAJECTORY DESIGN OF SILENT SUPERSONIC TECHNOLOGY DEMONSTRATOR (S3TD) |
ICAS 2008-5.7.5 |
| Suzuki, S. |
HARMONIZING AUTOMATION, PILOT AND AIR TRAFFIC CONTROLLER IN THE FUTURE AIR TRAFFIC MANAGEMENT |
ICAS 2008-8.2.4 |
| Suzuki, S. |
RESEARCH AND DEVELOPMENT FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM – PART 1. INTELLIGENT FLIGHT CONTROL SYSTEM |
ICAS 2008-5.10.1 |
| Suzuki, S. |
ROBUST OPTIMAL DESIGN OF AN AUTOPILOT FOR TRANSITIONAL FLIGHTS OF A TAIL-SITTER MINI UAV |
ICAS 2008-5.9.2 |
| Sweers, G. J. |
RECENT DEVELOPMENTS OF MSG-3 (MAINTANANCE STEERING GROUP) GUIDANCE FOR THE CONTINUED AIRWORTHINESS OF LIGHTNING/HIRF PROTECTION AND BENFITS TO NEW AIRPLANE DESIGN |
ICAS 2008-9.4.5 (AIAA 2008-8964 ) |
| Szasz, S. |
DESIGN OF EXPERIMENT FOR THE PILOT EVALUATION OF AN AIRBORNE RUNWAY INCURSION ALERTING SYSTEM |
ICAS 2008-9.10.2 |
| Szilder, K. |
PREDICTION OF SUPERCOOLED DROPLET IMPINGEMENT ON HELICOPTER ROTOR BLADES |
ICAS 2008-2.6.4 |
| Szurgyi, S. |
DEFINITION AND DEMONSTRATION OF THE AIRCRAFT PERFORMANCE EVALUATION CAPABILITIES (APECS) TOOL |
ICAS 2008-11.2.3 (AIAA 2008-8859) |
| Tabary, P. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
| Tafferner, A. |
AN INTEGRATED USER-ORIENTED WEATHER FORECAST SYSTEM FOR AIR TRAFFIC USING REAL-TIME OBSERVATIONS AND MODEL DATA |
ICAS 2008-8.6.3 |
| Tafferner, A. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
| Tahk, M. J |
NONLINEAR FORMATION GUIDANCE LAW WITH ROBUST DISTURBANCE OBSERVER |
ICAS 2008-5.7.4 |
| Tahk, M. J. |
INTEGRATED INTERCEPT MISSILE GUIDANCE AND CONTROL WITH TERMINAL ANGLE CONSTRAINT |
ICAS 2008-5.7.3 |
| Tahk, M. J. |
OPTIMIZATION FOR FLIGHT CONTROL SYSTEM WITH CONSTRAINTS SUPPLEMENTED HANDLING QUALITIES |
ICAS 2008-5.3.4 |
| Tahk, M. J. |
PERFORMANCE EVALUATION AND HILS TEST OF CONTROL ALLOCATION METHODS FOR RECONFIGURATION CONTROL |
ICAS 2008-5.10.3 |
| Takagi, S. |
RELATION BETWEEN TRAILING EDGE NOISE AND BOUNDARY LAYER INSTABILITY |
ICAS2008-P2.14 |
| Takeda, N. |
RECENT DEVELOPMENT OF STRUCTURAL HEALTH MONITORING TECHNOLOGIES FOR AIRCRAFT COMPOSITE STRUCTURES |
ICAS 2008-0.7 |
| Takenaka, K. |
MULTI-DISCIPLINARY DESIGN EXPLORATION FOR WINGLET |
ICAS 2008-1.1.3 |
| Tamada, I. |
NUMERICAL STUDY OF THE EFFECT OF THE OPPOSING JET ON REDUCTION OF AERODYNAMIC HEATING WITH DIFFERENT NOSE CONFIGURATIONS |
ICAS 2008-3.6.3 |
| Tan, X. |
LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
| Tanaka, H. |
DEVELOPMENT OF AN ONBOARD DOPPLER LIDAR FOR FLIGHT SAFETY |
ICAS 2008-9.9.2 |
| Tanaka, K. |
OVERVIEW OF THE NUMERICAL SIMULATIONS OF THE HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL |
ICAS2008-2.2 ST: |
| Tandale, M. D. |
MODEL-BASED AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.1 (AIAA 2008-8907) |
| Tandale, M. D. |
QUEUEING NETWORK MODELS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.10.3 (AIAA 2008-8942) |
| Tandale, M. D. |
RAPID PREDICTION OF AIR TRAFFIC FOR TRAJECTORY BASED OPERATIONS |
ICAS2008-11.6 ST (AIAA 2008-8902) |
| Tang, F. C. |
THE APPLICATION OF SEMI-EMPIRICAL STORE RELEASE SIMULATION FOR THE OPTIMIZATION OF GRID SURVEY WIND TUNNEL TESTING |
ICAS 2008-3.1.3 |
| Tang, H. |
EXTENDING FMC TEST FOR FLIGHT SIMULATION AND FLIGHT EXPERIMENTS |
ICAS 2008-5.5.3 |
| Tang, N. |
TARGETING PODS EFFECTS ON STORE SEPARATION CHARACTERISTICS: A JOINT NRC-IAR/USNAVY CFD EFFORT |
ICAS 2008-2.9.2 |
| Tani, Y. |
CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION |
ICAS 2008-1.2.3 |
| Tani, Y. |
NUMERICAL STUDY OF THE EFFECT OF THE OPPOSING JET ON REDUCTION OF AERODYNAMIC HEATING WITH DIFFERENT NOSE CONFIGURATIONS |
ICAS 2008-3.6.3 |
| Taniguchi, H. |
ANALYSIS OF DEEPSTALL LANDING FOR UAV |
ICAS 2008-5.6.4 |
| Tarakan, R. |
AN AUTOMATED SIMULATION PILOT CAPABILITY TO SUPPORT ADVANCED AIR TRAFFIC CONTROLLER TRAINING |
ICAS 2008-10.5.3 (AIAA 2008-8897) |
| Tarkian, M. |
AIRCRAFT PARAMETRIC 3D MODELING AND PANEL CODE ANALYSIS FOR CONCEPTUAL DESIGN |
ICAS2008-P1.3 |
| Taylor, R. M. |
METHODOLOGY FOR THERMALLY INDUCED LOADING IN STRUCTURAL ANALYSIS ON THE F-35 LIGHTNING II |
ICAS 2008-7.11.1 |
| Teimouri, H. |
EFFECTS OF HIERARCHY ORDER ON NATURAL FREQUENCY AND VIBRATION TRANSMISSION OF SELF-SIMILAR TRUSSES |
ICAS2008-P3.9 |
| Tessier, F. J. Z. |
AIRCRAFT PARAMETRIC 3D MODELING AND PANEL CODE ANALYSIS FOR CONCEPTUAL DESIGN |
ICAS2008-P1.3 |
| Tessmer, J. |
COLLAPSE BEHAVIOR OF THIN-WALLED CFRP STRUCTURES DUE TO MATERIAL AND GEOMETRIC NONLINEARITIES–EXPERIMENTS AND SIMULATION |
ICAS 2008-7.11.3 |
| Tessmer, J. |
IMPACT RESISTANCE, DAMAGE TOLERANCE AND NON-DESTRUCTIVE DAMAGE DETECTION FOR SANDWICH STRUCTURES: ANALYSIS AND TESTING |
ICAS2008-7.5 ST: |
| Tessmer, J. |
MECHANICS OF COMPOSITES IN LIGHTWEIGHT STRUCTURES: EFFICIENT TESTING AND COMPUTATION ACCOUNTING FOR COMPLEX 3D BEHAVIOUR |
ICAS 2008-7.11.2 |
| Tessmer, J. |
THERMAL ASPECTS FOR COMPOSITE STRUCTURES - FROM MANUFACTURING TO IN-SERVICE PREDICTIONS |
ICAS 2008-7.9.4 |
| Thalin, P. |
PARAMETRIC MODELING OF AN ELECTRICAL TEST RIG FOR POWER OPTIMIZED AIRCRAFT ARCHITECTURES |
ICAS2008-6.6 ST (AIAA 2008-8973) |
| Thielecke, F. |
EVAPORATING COOLANT FOR ON-BOARD COOLING SYSTEMS WITH DIRECT CONDENSATION THROUGH AMBIENT AIR |
ICAS 2008-6.6.3 |
| Thielecke, F. |
MONITORING OF OSCILLATORY FAILURE CASES FOR THE REDUCTION OF STRUCTURAL LOADS IN AN AEROELASTIC AIRCRAFT |
ICAS 2008-7.7.2 |
| Thielecke, F. |
MULTIVARIABLE CONTROLLER DESIGN FOR A TRIMMABLE HORIZONTAL STABILIZER ACTUATOR WITH TWO PRIMARY LOAD PATHS |
ICAS 2008-6.4.2 |
| Thien, H.C. |
643 DEVELOPMENT OF A COAXIAL ROTOR MAV FOR INDOOR APPLICATION |
ICAS2008-P1.9 |
| Thipphavong, D. |
AUTOMATED SEPARATION ASSURANCE IN THE PRESENCE OF UNCERTAINTY |
ICAS 2008-8.11.1 |
| Thomas, D. G. |
DESIGN ANALYSIS OF AN AIRCRAFT PARACHUTE RECOVERY SYSTEM FOR VERY LIGHT JETS |
ICAS2008-1.11 ST (AIAA 2008-8949) |
| Thomas, D. G. |
DEVELOPMENT OF A LANDING DRAG CHUTE SYSTEM SYSTEM FOR VERY LIGHT JETS |
ICAS 2008-1.11.3 (AIAA 2008-8950) |
| Thomas, J. P. |
REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
| Thomas, R. L. |
DESIGN ANALYSIS OF AN AIRCRAFT PARACHUTE RECOVERY SYSTEM FOR VERY LIGHT JETS |
ICAS2008-1.11 ST (AIAA 2008-8949) |
| Thomas, R. L. |
DEVELOPMENT OF A LANDING DRAG CHUTE SYSTEM SYSTEM FOR VERY LIGHT JETS |
ICAS 2008-1.11.3 (AIAA 2008-8950) |
| Thomson, R. |
INVESTIGATION OF ADHESIVELY BONDED COMPOSITE STRUCTURE JOINTS |
ICAS 2008-7.2.1 |
| Thomson, R. S. |
THE DESIGN OF POSTBUCKLING COMPOSITE AEROSPACE STRUCTURES ACCOUNTING FOR DAMAGE INITIATION AND GROWTH |
ICAS 2008-7.3.2 |
| Thouault, N. |
AERODYNAMIC INVESTIGATIONS ON A GENERIC FAN-IN-WING CONFIGURATION |
ICAS 2008-3.5.1 |
| Tian, F. L. |
RESEARCH ON FUZZY LOGIC PIO DETECTOR |
ICAS 2008-5.4.5 |
| Tilmann, C. P. |
SUPERSONIC AIRCRAFT FORMATION FLYING TO INCREASE FLIGHT EFFICIENCY |
ICAS 2008-1.10.2 |
| Toebben, H. H. |
INNOVATIVE FUTURE AIR TRANSPORT SYSTEM: SIMULATION OF A FULLY AUTOMATED ATS |
ICAS 2008-8.4.5 |
| Tomita, H. |
RESEARCH AND DEVELOPMENT FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM - PART 2 FLIGHT EXPERIMENTS |
ICAS 2008-5.10.2 |
| Torkamani, S. |
SCALED DOWN MODELS FOR FREE VIBRATION ANALYSIS OF ORTHOGONALLY STIFFENED CYLINDRICAL SHELLS USING SIMILITUDE THEORY |
ICAS 2008-7.7.5 |
| Torres, J. |
ON-DEMAND SPECIAL USE AIRSPACE |
ICAS 2008-10.10.4 (AIAA 2008-8938) |
| Torres, L. A. B. |
DEVELOPMENT OF A SMALL UNMANNED AIR VEHICLE WITH MINIMUM SENSORS PHILOSOPHY |
ICAS2008-1.4 ST: |
| Towers, G. |
A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
| Townsend, S. |
COUPLED HIGH-FIDELITY ENGINE SYSTEM SIMULATION |
ICAS 2008-8.10.3 INVITED |
| Tranchero, B. |
ALTERNATIVE ENERGY BASED SYSTEMS FOR ADVANCED U.A.V.; THE “SAVE” PROJECT |
ICAS2008-6.6 ST: |
| Trapani, M. |
DEVELOPMENT OF A RUDDERLESS AEROELASTIC FIN TECHNOLOGY |
ICAS 2008-7.10.2 |
| Trimmel, M. |
IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
| Trot, G. |
PRELIMINARY GUIDELINES ON FLIGHT DECK PROCEDURES FOR VERY CLOSELY SPACED PARALLEL APPROACHES |
ICAS 2008-8.5.2 |
| Trujillo, A. |
INFORMATION REQUIREMENTS FOR SUPERVISORY AIR TRAFFIC CONTROLLERS IN SUPPORT OF A MID-TERM WAKE VORTEX DEPARTURE SYSTEM |
ICAS 2008-8.11.3 |
| Trunk, M. |
LONG TERM AIRCRAFT PROJECT AND TECHNOLOGY EVALUATION UNDER THE UNCERTAINTY OF FUTURE SCENARIOS |
ICAS 2008-1.3.4 |
| Tsach, S. |
INNOVATIVE APPROACH FOR FUTURE AIRCRAFT DEVELOPMENT AT IAI |
ICAS 2008-1.6.1 |
| Tsourdos, A. |
INTEGRATED INTERCEPT MISSILE GUIDANCE AND CONTROL WITH TERMINAL ANGLE CONSTRAINT |
ICAS 2008-5.7.3 |
| Tsuda, H. |
CBAQ: DEVELOPMENT OF CRM BEHAVIOR ANALYSIS METHOD FOR MISSION FLIGHT CREW TRAINING |
ICAS 2008-9.2.1 |
| Tunney, J. |
FLIGHT EVALUATION OF A COMPACT AIRBORNE TRACE GAS ANALYSIS SENSOR PROOF-OF-CONCEPT |
ICAS2008-P6.4 |
| Turner, M. |
COUPLED HIGH-FIDELITY ENGINE SYSTEM SIMULATION |
ICAS 2008-8.10.3 INVITED |
| Turp, D. |
NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
| Twig, D. |
ADVANCED METHODOLOGIES FOR AVERAGE PROBABILITY CALCULATION FOR AEROSPACE SYSTEMS |
ICAS 2008-9.3.3 |
| Tysell, L. |
EXPERIENCES OF GRID GENERATION AND STEADY/UNSTEADY VISCOUS COMPUTATIONS FOR COMPLEX GEOMETRIES |
ICAS 2008-2.5.2 |
| Uebersax, A. |
STATIC AND FATIGUE ANALYSIS OF AN UPPER WING SKIN WITH EXFOLIATION CORROSION |
ICAS 2008-7.4.1 |
| Unger, R. |
NUMERICAL ANALYSIS OF THIN-WALLED STRUCTURES IN HYPERSONIC FLOW REGIME |
ICAS 2008-3.6.1 |
| Unger, R. |
NUMERICAL SIMULATION OF AN OSCILLATING AND FLEXIBLE AIRFOIL FOR FLAPPING WING PROPULSION WITH FLUID-STRUCTURE INTERACTION |
ICAS 2008-7.10.4 |
| Ura, H. |
AEROACOUSTIC NOISE MEASUREMENTS IN AERODYNAMIC LOW-SPEED WIND TUNNELS |
ICAS 2008-3.2.3 |
| Ura, H. |
OVERVIEW OF THE NUMERICAL SIMULATIONS OF THE HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL |
ICAS2008-2.2 ST: |
| Urik, T. |
INNOVATIVE COMPOSITE STRUCTURES FOR SMALL AIRCRAFT |
ICAS2008-7.3 ST: |
| Urvoy, C. |
SIMULATOR EVALUATION OF A NOVEL SURFACE MOVEMENT AWARENESS AND ALERTING SYSTEM (SMAAS) FOR RUNWAY INCURSION AVOIDANCE |
ICAS 2008-11.11.2 (AIAA 2008-8959) |
| Usdrowski, S. |
TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
| Utsch, R. L. de F. P. |
580 A MULTIDISCIPLINARY OPTIMIZATION METHOD APPLIED TO AIRCRAFT DESIGN |
ICAS2008-P1.4 |
| Valmorisco, M. |
SAFE AUTOMATIC FLIGHT BACK AND LANDING OF AIRCRAFT (SOFIA) |
ICAS2008-9.7 ST: |
| van Dalen, F. |
AUTOMATING THE DEVELOPMENT PROCESS OF THERMOPLASTIC COMPOSITE SHEET RIBS USING KNOWLEDGE BASED ENG. TECHNIQUES |
ICAS 2008-6.10.3 |
| van Dartel, I. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
| van de Vijver, Y. A. J. R. |
ENVIRONMENT-AWARE RUNWAY ALLOCATION ADVICE SYSTEM |
ICAS 2008-4.11.2 |
| van den Hoven, M. |
A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
| van der Elst, S. W. G. |
DOMAIN SPECIFIC MODELING LANGUAGES TO SUPPORT MODEL-DRIVEN ENGINEERING OF AIRCRAFT SYSTEMS |
ICAS 2008-1.9.2 (AIAA 2008-8927) |
| van der Heul, D. R. |
OPTIMISING HIGH-EFFICIENCY RUDDERS FOR TRANSPORT AIRCRAFT FUEL BURN REDUCTION |
ICAS 2008-2.11.2 |
| van der Laan, T. |
AUTOMATING THE DEVELOPMENT PROCESS OF THERMOPLASTIC COMPOSITE SHEET RIBS USING KNOWLEDGE BASED ENG. TECHNIQUES |
ICAS 2008-6.10.3 |
| van der Steen, M. |
THE APPLICATION OF SEMI-EMPIRICAL STORE RELEASE SIMULATION FOR THE OPTIMIZATION OF GRID SURVEY WIND TUNNEL TESTING |
ICAS 2008-3.1.3 |
| Van der Velden, C. |
AN ADAPTABLE METHODOLOGY FOR AUTOMATION APPLICATION DEVELOPMENT |
ICAS 2008-6.2.3 |
| van der Wal, H. |
A NOVEL RECIPROCAL SOUND TRANSMISSION MEASURING METHOD, APPLIED ON A COMPOSITE FUSELAGE |
ICAS 2008-4.9.3 |
| van Eenige, M. J. A. |
A PRACTICAL APPROACH TO MULTI-OBJECTIVE CAPACITY ANALYSIS OF AN ENVIRONMENT-AWARE AIRPORT |
ICAS 2008-8.5.1 |
| van Gerwen, D. J. |
A NEW APPROACH TO FORCED FLAPPING FOR THE ORNICOPTER |
ICAS 2008-10.11.3 (AIAA 2008-8975) |
| van Holten, T. |
A NEW APPROACH TO FORCED FLAPPING FOR THE ORNICOPTER |
ICAS 2008-10.11.3 (AIAA 2008-8975) |
| van Holten, T. |
FEASIBILITY ANALYSIS OF ACHIEVING A STABILIZED APPROACH |
ICAS 2008-5.4.2 |
| van Muijden, J. |
EFFICIENT AEROELASTIC SIMULATION IN A PARAMETRIC PROCEDURE FOR FATIGUE ANALYSIS |
ICAS 2008-7.7.1 |
| Van Putten, B. -J. |
AN ONTOLOGY FOR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-9.11.1 (AIAA 2008-8946) |
| van Tooren, M. J. L. |
DEVELOPMENT AND IMPLEMENTATION OF KNOWLEDGE-BASED DESIGN PROCESS PRIMITIVES |
ICAS 2008-6.10.4 |
| van Tooren, M. J. L. |
DOMAIN SPECIFIC MODELING LANGUAGES TO SUPPORT MODEL-DRIVEN ENGINEERING OF AIRCRAFT SYSTEMS |
ICAS 2008-1.9.2 (AIAA 2008-8927) |
| van Tooren, M. J. L. |
KNOWLEDGE BASED ENGINEERING TO SUPPORT AIRCRAFT MULTIDISCIPLINARY DESIGN AND OPTIMISATION |
ICAS 2008-6.10.1 |
| Van Tooren, M. J. L. |
MDO DESIGN SUPPORT BY INTEGRATED ENGINEERING SERVICES WITHIN A MULTI-AGENT TASK ENVIRONMENT |
ICAS 2008-1.11.1 (AIAA 2008-8947) |
| Vankan, W. J. |
A PRACTICAL APPROACH TO MULTI-OBJECTIVE CAPACITY ANALYSIS OF AN ENVIRONMENT-AWARE AIRPORT |
ICAS 2008-8.5.1 |
| Vargas, F. J. T. |
A PROCEDURE TO DESIGN AIRCRAFT FLIGHT CONTROL LAWS TAKING INTO ACCOUNT ROBUSTNESS USING THE VARIABLE STRUCTURE CONTROL |
ICAS2008-5.4 ST: |
| Veldhuis, L. L. M. |
PROPELLER SLIPSTREAM INVESTIGATION USING THE FOKKER F27 WIND TUNNEL MODEL WITH FLAPS DEFLECTED |
ICAS 2008-3.1.2 |
| Veldhuis, L. L. M. |
VORTEX WAKE INVESTIGATION BEHIND A WING-FLAP MODEL WITH JET SIMULATION |
ICAS 2008-3.9.1 |
| Vera-Morales, M. |
NETWORK AND ENVIRONMENTAL IMPACTS OF PASSENGER AND AIRLINE RESPONSE TO COST AND DELAY |
ICAS 2008-10.4.4 (AIAA 2008-8890) |
| Veress, A. |
FEASIBILITY STUDY ON MULTI-PHASE FLOW SIMULATION OF FUEL INJECTION USING LATTICE BOLTZMANN METHOD |
ICAS 2008-4.3.4 |
| Verhoeff, L. |
ENABLING TECHNOLOGY EVALUATION FOR EFFICIENT CONTINUOUS DESCENT APPROACHES |
ICAS 2008-8.9.2 |
| Verhoeven, R. P. M. |
ENABLING TECHNOLOGY EVALUATION FOR EFFICIENT CONTINUOUS DESCENT APPROACHES |
ICAS 2008-8.9.2 |
| Verhoeven, R. P. M. |
NATIONAL TECHNOLOGY PROJECT 'OUTCAST' ON UAV SENSE AND AVOID |
ICAS 2008-8.1.2 |
| Verma, S. |
PRELIMINARY GUIDELINES ON FLIGHT DECK PROCEDURES FOR VERY CLOSELY SPACED PARALLEL APPROACHES |
ICAS 2008-8.5.2 |
| Vermeulen, B. |
AUTOMATING THE DEVELOPMENT PROCESS OF THERMOPLASTIC COMPOSITE SHEET RIBS USING KNOWLEDGE BASED ENG. TECHNIQUES |
ICAS 2008-6.10.3 |
| Vernaleken, C. |
SIMULATOR EVALUATION OF A NOVEL SURFACE MOVEMENT AWARENESS AND ALERTING SYSTEM (SMAAS) FOR RUNWAY INCURSION AVOIDANCE |
ICAS 2008-11.11.2 (AIAA 2008-8959) |
| Verstraete, D. |
AN ASSESSMENT OF THE POTENTIAL OF HYDROGEN FUELED LARGE LONG-RANGE TRANSPORT AIRCRAFT |
ICAS 2008-1.2.4 |
| Verstraete, D. |
PRELIMINARY DESIGN OF A JOINED WING HALE UAV |
ICAS 2008-1.4.3 |
| Vesely, L. |
THE EFFECTS OF WALL ROUGHNESS ON THE TURBULENT BOUNDARY LAYER |
ICAS 2008-3.8.1 |
| Veul, R. P. G. |
EFFICIENT AEROELASTIC SIMULATION IN A PARAMETRIC PROCEDURE FOR FATIGUE ANALYSIS |
ICAS 2008-7.7.1 |
| Vian, J. |
HEALTH MONITORING FOR COMMERCIAL AIRCRAFT SYSTEMS |
ICAS 2008-6.1.2 |
| Vieillard, S. |
HIGH EFFICIENCY, HIGH RELIABILITY 2 KW INVERTER FOR AERONAUTICAL APPLICATION |
ICAS 2008-6.1.3 |
| Viola, N. |
ALTERNATIVE ENERGY BASED SYSTEMS FOR ADVANCED U.A.V.; THE “SAVE” PROJECT |
ICAS2008-6.6 ST: |
| Visser, H. G. |
OPTIMIZATION OF RNAV NOISE ABATEMENT ARRIVAL TRAJECTORIES |
ICAS 2008-4.11.1 |
| Vitic, A. |
PROTOTYPE OF A STIFF WIND TUNNEL BALANCE WITH SEMICONDUCTOR STRAIN GAUGES AND THERMOCOMPENSATION DONE BY SOFTWARE |
ICAS2008-P2.9 |
| Viviani, A. |
ANALYSIS OF THERMOCHEMICAL MODELING AND SURFACE CATALYTICITY IN SPACE VEHICLES REENTRY |
ICAS 2008-3.6.2 |
| von Kaenel, R. |
CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
| Vos, J. |
UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
| Vos, R. |
POST-BUCKLED PRECOMPRESSED ELEMENTS: A NEW CLASS OF FLIGHT CONTROL ACTUATORS ENHANCING MORPHING WING UAVS |
ICAS 2008-7.8.2 |
| Voskuijl, M. |
CONTROLLABILITY OF BLENDED WING BODY AIRCRAFT |
ICAS 2008-5.4.3 |
| Vu, K. -P. L. |
COMPARING SITUATION AWARENESS MEASUREMENT TECHNIQUES IN A LOW FIDELITY AIR TRAFFIC CONTROL SIMULATION |
ICAS 2008-9.7.4 |
| Vukovic, D. |
PROTOTYPE OF A STIFF WIND TUNNEL BALANCE WITH SEMICONDUCTOR STRAIN GAUGES AND THERMOCOMPENSATION DONE BY SOFTWARE |
ICAS2008-P2.9 |
| Wachendorf, N. |
MULTIVARIABLE CONTROLLER DESIGN FOR A TRIMMABLE HORIZONTAL STABILIZER ACTUATOR WITH TWO PRIMARY LOAD PATHS |
ICAS 2008-6.4.2 |
| Wadia, A. |
NUMERICAL INVESTIGATION OF INLET DISTORTION INDUCED SWIRL IN MULTISTAGE FANS |
ICAS 2008-4.4.3 |
| Wagner, C. |
SCALING OF MIXED CONVECTION IN AIRCRAFT CABINS |
ICAS 2008-6.3.3 |
| Waitz, I. |
ENVIRONMENTAL IMPACT OF AVIATION: A REVIEW OF SELECTED US RESEARCH EFFORTS |
ICAS 2008-0.2 |
| Waitz, I. |
INTERDEPENDENCIES IN LOCAL AIR QUALITY AND NOISE IMPACTS FOR LANDING AND TAKEOFF OPERATIONS |
ICAS 2008-11.3.2 (AIAA 2008-8866) |
| Wallin, M. |
COMPRESSION STRENGTH OF NOTCHED AND IMPACT DAMAGED COMPOSITE LAMINATES |
ICAS 2008-7.5.2 |
| Walther, R. |
CUTTING EDGE TECHNOLOGIES FOR DESIGN, PRODUCTION AND REPAIR OF NEXT GENERATION AERO ENGINES |
ICAS 2008-8.10.2 INVITED |
| Wan, F. Y. |
HEALTH MONITORING FOR AEROCRAFT STRUCTURE SYSTEM BY HARMONIC WAVELET TRANSFORM |
ICAS2008-7.7 ST: |
| Wan, T. |
NUMERICAL SIMULATION OF FLAPPING WING AERODYNAMIC PERFORMANCE UNDER GUST WIND CONDITIONS |
ICAS2008-3.5 ST: |
| Wan, T. |
THE IMPLEMENTATION OF ANALYTICAL HIERARCHY PROCESS IN FLIGHT SAFETY |
ICAS 2008-9.2.4 |
| Wang, J. |
LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
| Wang, J. A. |
DEVELOPMENT OF FLIGHT CONTROL SYSTEM USING EMBEDDED COMPUTER PC-104 |
ICAS2008-P5.1 |
| Wang, J.- G. |
15 THE SIGNAL-TO-NOISE RATIO MODELING OF RADAR IN ELECTRONIC COUNTER-COUNTER MEASURES |
ICAS2008-P6.7 |
| Wang, L. |
3 A STUDY ON FATIGUE SCATTER FACTOR OF INDIVIDUAL AIRCRAFT STRUCTURE |
ICAS2008-P3.1 |
| Wang, L. |
FATIGUE BEHAVIOR AND LIFE PREDICTION OF WELDED TITANIUM ALLOY JOINTS |
ICAS 2008-7.4.4 |
| Wang, S. |
EXTENDING FMC TEST FOR FLIGHT SIMULATION AND FLIGHT EXPERIMENTS |
ICAS 2008-5.5.3 |
| Wang, X. |
METHODS FOR CALCULATING THE DAMAGE-RATE OF AIRCRAFT COMPONENT |
ICAS2008-9.8 ST: |
| Wang, Y. |
A LAYER PAVEMENT MODEL TO SIMULATE ROUGHNESS FEATURES IN ICE ACCRETION NUMERICAL SIMULATION |
ICAS 2008-2.6.1 |
| Wang, Z. |
64 A PROGRAM OF AIRCRAFT EQUIPMENT AND SUBSYSTEMS LIFE EXTENSION |
ICAS2008-P6.1 |
| Wang, Z. |
3 A STUDY ON FATIGUE SCATTER FACTOR OF INDIVIDUAL AIRCRAFT STRUCTURE |
ICAS2008-P3.1 |
| Wang, Z. |
ANALYSIS OF THE SCATTERING CHARACTERISTICS FROM DISCONTINUITY SURFACES ON AIRCRAFT USING A MODIFIED MLFMA |
ICAS2008-P3.6 |
| Wanke, C. |
METHODOLOGIES FOR ESTIMATING THE IMPACT OF SEVERE WEATHER ON AIRSPACE CAPACITY |
ICAS 2008-10.7.4 (AIAA 2008-8917) |
| Webb, L. |
KNOWLEDGE MANAGEMENT FOR THROUGH LIFE SUPPORT |
ICAS 2008-6.11.3 |
| Weigel, A. L. |
PRELIMINARY ANALYSIS OF STRATEGIES AND CHALLENGES TO ENCOURAGE DATA LINK ADOPTION OVER THE NORTH ATLANTIC AIRSPACE |
ICAS 2008-8.8.3 (AIAA 2008-8953) |
| Welch, B. |
AUTOMATED ASSEMBLY TIME ANALYSIS USING A DIGITAL KNOWLEDGE BASED APPROACH |
ICAS 2008-10.3.1 (AIAA 2008-8861) |
| Welch, B. |
USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
| Wen, X. |
THE APPLICATION OF AIRBORNE VIDEO TECHNOLOGIES DURING AERIAL REFUELING TEST |
ICAS2008-P5.2 |
| Westhoff, A. |
SCALING OF MIXED CONVECTION IN AIRCRAFT CABINS |
ICAS 2008-6.3.3 |
| Weston, N. |
AN APPROACH FOR MULTI-CRITERIA DECISION MAKING METHOD SELECTION AND DEVELOPMENT |
ICAS 2008-1.3.1 |
| Wetzel, A. |
IMPACT RESISTANCE, DAMAGE TOLERANCE AND NON-DESTRUCTIVE DAMAGE DETECTION FOR SANDWICH STRUCTURES: ANALYSIS AND TESTING |
ICAS2008-7.5 ST: |
| Wheeler, P. W. |
A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
| White, B. A. |
INTEGRATED INTERCEPT MISSILE GUIDANCE AND CONTROL WITH TERMINAL ANGLE CONSTRAINT |
ICAS 2008-5.7.3 |
| Whitley, C. |
A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
| Whitlow Jr., W. |
PROPULSION TECHNOLOGIES FOR THE FUTURE OF AVIATION |
ICAS 2008-8.10.5 INVITED |
| Wijekoon, T. |
A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
| Wiklund, P. -E. |
VIRTUAL ENTERPRISE COLLABORATION - BREAKTHROUGH TECHNOLOGIES PROVIDED BY VIVACE |
ICAS 2008-8.10.4 INVITED |
| Wild, J. |
NUMERICAL AERODYNAMIC OPTIMISATIONS OF 3D HIGH-LIFT CONFIGURATIONS |
ICAS 2008-2.2.3 |
| Wildschek, A. |
MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
| Wille, T. |
THERMAL ASPECTS FOR COMPOSITE STRUCTURES - FROM MANUFACTURING TO IN-SERVICE PREDICTIONS |
ICAS 2008-7.9.4 |
| Willems, B. |
RELATIONSHIP OF MAXIMUM MANAGEABLE AIR TRAFFIC CONTROL COMPLEXITY AND SECTOR CAPACITY |
ICAS 2008-8.2.3 |
| Williams, D. |
INFORMATION REQUIREMENTS FOR SUPERVISORY AIR TRAFFIC CONTROLLERS IN SUPPORT OF A MID-TERM WAKE VORTEX DEPARTURE SYSTEM |
ICAS 2008-8.11.3 |
| Williams, D. |
WAKE TURBULENCE MITIGATION FOR ARRIVALS (WTMA) |
ICAS 2008-9.9.3 |
| Willis, D. J. |
COMPUTATIONAL INVESTIGATION AND DESIGN OF COMPLIANT MEMBRANE WINGS FOR BIOLOGICALLY INSPIRED FLIGHT VEHICLES |
ICAS 2008-2.10.1 |
| Wilson, A. |
NUMERICAL STUDY OF ENERGY UTILIZATION IN NOZZLE/PLUME FLOW-FIELDS OF HIGH-SPEED AIR-BREATHING VEHICLES |
ICAS 2008-4.3.3 |
| Winckelmans, G. |
PILOTED SIMULATION RESULTS OF AN ONBOARD WAKE VORTEX DETECTION, WARNING AND AVOIDANCE SYSTEM AND COCKPIT DISPLAY ASPECTS |
ICAS 2008-9.9.1 |
| Wing, D. J. |
PERFORMANCE BASIS FOR AIRBORNE SEPARATION |
ICAS 2008-8.7.1 |
| Winkler, C. |
A HYBRID, DYNAMIC LARGE EDDY SIMULATION METHOD |
ICAS 2008-2.1.1 |
| Wolfe, S. R. |
AN ONTOLOGY FOR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-9.11.1 (AIAA 2008-8946) |
| Won, H. T. |
ADVANCED GENERAL AVIATION DESIGN WITH TRANSPORTATION ARCHITECTURE ANALYSIS |
ICAS 2008-1.9.4 (AIAA 2008-8929) |
| Wong, H. M. |
THE FEASIBILITY AND POTENTIAL ENVIRONMENTAL BENEFITS OF ALTERNATIVE FUELS FOR COMMERCIAL AVIATION |
ICAS 2008-4.7.5 |
| Wood, B. |
MICROSCOPIC ANALYSIS OF AIRPORT SURFACE SEQUENCING |
ICAS2008-11.11 ST (AIAA 2008-8961) |
| Worden, K. |
A NEGATIVE SELECTION APPROACH TO DETECT DAMAGE IN AERONAUTICAL STRUCTURES WITH CHANGING OPERATING CONDITIONS |
ICAS 2008-9.4.2 |
| Wroblewski, W. |
THE INFLUENCE OF FREE - PLAY AND FRICTION IN CONTROL SYSTEM ON AIRCRAFT DYNAMICS |
ICAS 2008-5.10.5 |
| Wu, C. |
TERRAIN FOLLOWING FLIGHT REAL-TIME HIL SIMULATION PLATFORM RESEARCH |
ICAS2008-P5.6 |
| Wu, D. |
AERODYNAMICS CHARACTERISTICS OF HYPERSONIC VEHICLE IN NEAR SPACE |
ICAS2008-2.5 ST: |
| Wu, L. |
STUDY ON THE RELATIONSHIP BETWEEN CORROSION DAMAGE AND RESIDUAL STRENGTH OF AL 7075-T6 ALLOY |
ICAS 2008-9.8.2 |
| Wu, X.-R. |
FATIGUE BEHAVIOR AND LIFE PREDICTION OF WELDED TITANIUM ALLOY JOINTS |
ICAS 2008-7.4.4 |
| Wu, Z. |
AN UPDATING PROGRAM FOR UNDERGRADUATE AIRCRAFT CONCEPTUAL AND PRELIMINARY DESIGN COURSE |
ICAS2008-P1.5 |
| Xia, L. |
THE APPLICATION OF ASEXUAL DNA ALGORITHM TO AIRFOIL DESIGN |
ICAS 2008-2.3.3 |
| Xiao, H. |
AERODYNAMICS CHARACTERISTICS OF HYPERSONIC VEHICLE IN NEAR SPACE |
ICAS2008-2.5 ST: |
| Xiong, J. T. |
AERODYNAMIC SHAPE OPTIMIZATION OF TRANSONIC AEROELASTIC WING BASED ON CONTROL THEORY |
ICAS2008-9.6 ST: |
| Xu, H. |
PREDICTION OF SUPERCOOLED DROPLET IMPINGEMENT ON HELICOPTER ROTOR BLADES |
ICAS 2008-2.6.4 |
| Xu, Y. |
LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
| Xue, H. J. |
ERGONOMIC ASSESSMENT METHOD FOR COCKPIT LAYOUT OF CIVIL AIRCRAFT X BASED ON VIRTUAL DESIGN |
ICAS2008-P6.5 |
| Xue, H. J. |
THE SIMULATION OF THE HUMAN-MACHINE PARTNERSHIP IN UCAV OPERATION |
ICAS 2008-9.10.5 |
| Xue, J. |
EFFECTS OF SUSPENSION WEIGHT ON FIGHTER FATIGUE DAMAGE |
ICAS 2008-7.4.5 |
| Yadlin, Y. |
FLOW CONTROL TECHNIQUES FOR TRANSPORT AIRCRAFT |
ICAS 2008-3.11.1 |
| Yamada, H. |
DEVELOPMENT OF FULL ANNULAR COMBUSTOR FOR SMALL AIRCRAFT JET ENGINE IN JAXA TECHCLEAN PROJECT |
ICAS 2008-4.3.2 |
| Yamamoto, K. |
COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA |
ICAS 2008-2.2.1 |
| Yamamoto, K. |
INVESTIGATION OF THE FLOW OVER NACELLE/PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION |
ICAS 2008-3.3.3 |
| Yamamoto, K. |
OVERVIEW OF THE NUMERICAL SIMULATIONS OF THE HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL |
ICAS2008-2.2 ST: |
| Yamamoto, T. |
DEVELOPMENT OF FULL ANNULAR COMBUSTOR FOR SMALL AIRCRAFT JET ENGINE IN JAXA TECHCLEAN PROJECT |
ICAS 2008-4.3.2 |
| Yamashita, H. |
COMPARISON OF SHOCK WAVE INTERACTION FOR THE THREE-DIMENSIONAL SUPERSONIC BIPLANE WITH DIFFERENT PLANAR SHAPES |
ICAS 2008-2.4.5 |
| Yamashita, H. |
LOW-BOOM AND LOW-DRAG OPTIMIZATION FOR THE TWIN-ENGINE SILENT SUPERSONIC TECHNOLOGY DEMONSTRATOR |
ICAS 2008-2.4.1 |
| Yamashita, H. |
WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION |
ICAS2008-2.4 ST: |
| Yan, S. W. |
RESEARCH ON FUZZY LOGIC PIO DETECTOR |
ICAS 2008-5.4.5 |
| Yan, Y. |
NUMERICAL SIMULATION OF FORMING PROCESS OF AIRCRAFT TRANSPARENCIES MANUFACTURED BY POLYMERIC PLATE |
ICAS2008-P7.1 |
| Yanagida, A. |
RESEARCH AND DEVELOPMENT FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM – PART 1. INTELLIGENT FLIGHT CONTROL SYSTEM |
ICAS 2008-5.10.1 |
| Yanagida, A. |
RESEARCH AND DEVELOPMENT FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM - PART 2 FLIGHT EXPERIMENTS |
ICAS 2008-5.10.2 |
| Yang, E. -S. |
DEMAND-CENTRIC ANALYSIS OF THE AIR TRANSPORTATION SYSTEM |
ICAS 2008-10.4.3 (AIAA 2008-8889) |
| Yang, W. Q. |
NUMERICAL SIMULATION OF 3D FLAPPING WING BASED ON CHIMERA METHOD |
ICAS 2008-2.10.5 |
| Yang, X. D. |
AERODYNAMIC SHAPE OPTIMIZATION OF TRANSONIC AEROELASTIC WING BASED ON CONTROL THEORY |
ICAS2008-9.6 ST: |
| Yao, J. |
NUMERICAL INVESTIGATION OF INLET DISTORTION INDUCED SWIRL IN MULTISTAGE FANS |
ICAS 2008-4.4.3 |
| Yao, Z. X. |
MISSION DECISION-MAKING METHOD OF MULTI-AIRCRAFT COOPERATIVELY ATTACKING MULTI-TARGET BASED ON SITUATIONAL ASSESSMENT |
ICAS2008-P1.2 |
| Yarf-Abbasi, A. |
DESIGN AND DEVELOPMENT OF THE ECLIPSE AND DEMON DEMONSTRATOR UAVS |
ICAS 2008-1.4.2 |
| Yashin, Y. |
THEORETICAL APPROACH TO DIRECTIONAL CONTROL SENSITIVITY SELECTION |
ICAS 2008-5.4.1 INVITED |
| Yayama, T. |
CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION |
ICAS 2008-1.2.3 |
| Ye, K. D. |
IDENTIFYING FATIGUE OF FLIGHT ATTENDANTS IN SHORT-HAUL OPERATIONS |
ICAS 2008-9.2.3 |
| Ye, Z. |
NUMERICAL RESEARCHES ON THE AEROELASTIC PROBLEM OF TURBOMACHINERY |
ICAS 2008-4.4.4 |
| Yen, J -R. |
IDENTIFYING FATIGUE OF FLIGHT ATTENDANTS IN SHORT-HAUL OPERATIONS |
ICAS 2008-9.2.3 |
| Yimer, I. |
DEVELOPMENT OF AN INDUSTRIAL SCALE COMBUSTION TEST AND RESEARCH FACILITY FOR ALTERNATIVE FUELS AND FUEL FLEXIBILITY DEMONSTRATION |
ICAS 2008-4.3.1 |
| Yin, Y. |
USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
| Yokokawa, Y. |
AEROACOUSTIC NOISE MEASUREMENTS IN AERODYNAMIC LOW-SPEED WIND TUNNELS |
ICAS 2008-3.2.3 |
| Yokokawa, Y. |
COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA |
ICAS 2008-2.2.1 |
| Yokokawa, Y. |
INVESTIGATION OF THE FLOW OVER NACELLE/PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION |
ICAS 2008-3.3.3 |
| Yokokawa, Y. |
OVERVIEW OF THE NUMERICAL SIMULATIONS OF THE HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL |
ICAS2008-2.2 ST: |
| Yonezawa, M. |
COMPARISON OF SHOCK WAVE INTERACTION FOR THE THREE-DIMENSIONAL SUPERSONIC BIPLANE WITH DIFFERENT PLANAR SHAPES |
ICAS 2008-2.4.5 |
| Yonezawa, M. |
LOW-BOOM AND LOW-DRAG OPTIMIZATION FOR THE TWIN-ENGINE SILENT SUPERSONIC TECHNOLOGY DEMONSTRATOR |
ICAS 2008-2.4.1 |
| Yonezawa, M. |
WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION |
ICAS2008-2.4 ST: |
| York, C. B. |
APPROXIMATIONS FOR FULLY ISOTROPIC LAMINATE CONFIGURATIONS |
ICAS 2008-7.3.1 |
| Yoshida, K. |
FLIGHT TEST RESULTS AT TRANSONIC REGION ON SUPERSONIC EXPERIMENTAL AIRPLANE (NEXST-1) |
ICAS 2008-2.4.2 |
| Young, J. |
FLAPPING-WING TECHNOLOGY: THE POTENTIAL FOR AIR VEHICLE PROPULSION AND AIRBORNE POWER GENERATION |
ICAS 2008-1.5.1 |
| Young, T. M. |
SIMPLIFIED METHODS FOR ASSESSING THE IMPACT OF FUEL ENERGY CONTENT ON PAYLOAD-RANGE |
ICAS 2008-11.2.1 (AIAA 2008-8857) |
| Yu, T. X. |
HEALTH MONITORING FOR AEROCRAFT STRUCTURE SYSTEM BY HARMONIC WAVELET TRANSFORM |
ICAS2008-7.7 ST: |
| Yu, X. |
AN ADAPTABLE METHODOLOGY FOR AUTOMATION APPLICATION DEVELOPMENT |
ICAS 2008-6.2.3 |
| Yuan, W. |
A CFD STUDY OF UCAV 1303 BASELINE MODEL AT CRUISE MACH NUMBERS |
ICAS 2008-2.5.1 |
| Yun, S. |
DEVELOPMENT OF AN INDUSTRIAL SCALE COMBUSTION TEST AND RESEARCH FACILITY FOR ALTERNATIVE FUELS AND FUEL FLEXIBILITY DEMONSTRATION |
ICAS 2008-4.3.1 |
| Zabloudil, M. |
WIND TUNNEL AND COMPUTIONAL INVESTIGATION OF SIMULATED CONTAMINATION ON AIRFOIL |
ICAS2008-P2.11 |
| Zaichik, L. |
THEORETICAL APPROACH TO DIRECTIONAL CONTROL SENSITIVITY SELECTION |
ICAS 2008-5.4.1 INVITED |
| Zakrzewski, E. |
TERMINAL AREA REQUIRED TIME OF ARRIVAL (RTA) CONCEPT OF OPERATIONS AND AUTOMATION PROTOTYPE |
ICAS 2008-11.9.1 (AIAA 2008-8930) |
| Zammit, A. |
BIRD-STRIKE DAMAGE ANALYSIS IN CONCEPT ADVANCED COMPOSITE FAN BLADES |
ICAS 2008-4.4.1 |
| Zammit, B. |
DESIGN OF EXPERIMENT FOR THE PILOT EVALUATION OF AN AIRBORNE RUNWAY INCURSION ALERTING SYSTEM |
ICAS 2008-9.10.2 |
| Zammit-Mangion, D. |
A RAPID SCENARIO GENERATION TOOL FOR REPEATABLE SIMULATED TRAFFIC CONFLICTS IN FLIGHT SIMULATION |
ICAS 2008-5.1.1 INVITED |
| Zammit-Mangion, D. |
DESIGN OF EXPERIMENT FOR THE PILOT EVALUATION OF AN AIRBORNE RUNWAY INCURSION ALERTING SYSTEM |
ICAS 2008-9.10.2 |
| Zelinski, S. |
DEFINING DYNAMIC CRITICAL POINTS FOR DYNAMIC AIRSPACE CONFIGURATION |
ICAS 2008-8.9.3 |
| Zhan, H. |
THE APPLICATION OF ASEXUAL DNA ALGORITHM TO AIRFOIL DESIGN |
ICAS 2008-2.3.3 |
| Zhang, C. |
NUMERICAL RESEARCHES ON THE AEROELASTIC PROBLEM OF TURBOMACHINERY |
ICAS 2008-4.4.4 |
| Zhang, D. |
TEST DATA MANAGEMENT FOR AIRCRAFT HYDRAULIC SYSTEM TESTING |
ICAS2008-P6.3 |
| Zhang, D. G. |
NUMERICAL SIMULATION OF FORMING PROCESS OF AIRCRAFT TRANSPARENCIES MANUFACTURED BY POLYMERIC PLATE |
ICAS2008-P7.1 |
| Zhang, F. |
A CFD STUDY OF UCAV 1303 BASELINE MODEL AT CRUISE MACH NUMBERS |
ICAS 2008-2.5.1 |
| Zhang, G. L. |
NUMERICAL SIMULATION OF FORMING PROCESS OF AIRCRAFT TRANSPARENCIES MANUFACTURED BY POLYMERIC PLATE |
ICAS2008-P7.1 |
| Zhang, H. |
64 A PROGRAM OF AIRCRAFT EQUIPMENT AND SUBSYSTEMS LIFE EXTENSION |
ICAS2008-P6.1 |
| Zhang, J. F. |
275 IMPACT AND COMPRESSION-AFTER-IMPACT PERFORMANCE OF STITCHED/UNSTITCHED COMPOSITE SANDWICH PANELS WITH A FOAM CORE |
ICAS2008-P3.7 |
| Zhang, W. |
THE NUMERICAL SIMULATION ANALYSIS OF KEY STRUCTURES OF INTEGRATED POWER SUPPLY IN MOTOR-PUMP |
ICAS2008-P6.2 |
| Zhang, Y. F. |
DEVELOPMENT OF FLAPPING WING MICRO AIR VEHICLE |
ICAS 2008-1.5.3 |
| Zhang, Y. Z. |
DEVELOPMENT OF FLAPPING WING MICRO AIR VEHICLE |
ICAS 2008-1.5.3 |
| Zhao, G. |
THE SYSTEM FAULT BEHAVIOR AND MODEL |
ICAS2008-P9.2 |
| Zhao, G. Y. |
THE SYSTEM FAULT BEHAVIOR AND MODEL |
ICAS2008-P9.2 |
| Zhao, Y. J. |
A SYSTEMATIC PROCEDURE FOR DETERMINING SEPARATION MINIMA |
ICAS 2008-8.7.4 |
| Zheng, X. T. |
275 IMPACT AND COMPRESSION-AFTER-IMPACT PERFORMANCE OF STITCHED/UNSTITCHED COMPOSITE SANDWICH PANELS WITH A FOAM CORE |
ICAS2008-P3.7 |
| Zhou, Y. M. |
THE APPLICATION OF THE MORLET WAVELET ON RESPONSE FILTERING OF THE HELICOPTER CANNON’S RECOIL |
ICAS2008-P3.5 |
| Zhu, B. |
TRANSONIC FLUTTER ANALYSIS OF AN AIRFOIL WITH APPROXIMATE BOUNDARY METHOD |
ICAS 2008-7.10.5 |
| Zhu, Q. |
EFFECTS OF SUSPENSION WEIGHT ON FIGHTER FATIGUE DAMAGE |
ICAS 2008-7.4.5 |
| Zhu, Y. |
15 THE SIGNAL-TO-NOISE RATIO MODELING OF RADAR IN ELECTRONIC COUNTER-COUNTER MEASURES |
ICAS2008-P6.7 |
| Zobell, S. |
METHODOLOGIES FOR ESTIMATING THE IMPACT OF SEVERE WEATHER ON AIRSPACE CAPACITY |
ICAS 2008-10.7.4 (AIAA 2008-8917) |
| Zugaj, M. T. |
NONLINEAR MODEL FOLLOWING RECONFIGURABLE FLIGHT CONTROL SYSTEM |
ICAS 2008-5.10.4 |
| Zurek, J. |
MODELING AND SIMULATION OF FLAPPING WINGS MICRO-AERIAL VEHICLES FLIGHT DYNAMICS |
ICAS 2008-5.9.1 INVITED |
| Zurek, J. |
THE INFLUENCE OF FREE - PLAY AND FRICTION IN CONTROL SYSTEM ON AIRCRAFT DYNAMICS |
ICAS 2008-5.10.5 |