| TITLE |
PAPER NUMBER |
TOPIC |
| COLLABORATION CHALLENGES IN
THE GLOBAL AEROSPACE MARKET FOR SMALLER COUNTRIES - AN AUSTRALIAN PERSPECTIVE |
ICAS 2012-0.1 |
General Lectures |
| BEYOND
THE BLACK BOX: THE FORENSICS OF AIRPLANE CRASHES |
ICAS 2012-0.2 |
General Lectures |
| LESSONS LEARNED IN FULL
COMPOSITE AERO-STRUCTURES DEVELOPMENT IN JAPAN |
ICAS 2012-0.3 |
General Lectures |
| MULTIDISCIPLINARY AIRFRAME
DESIGN OPTIMIZATION |
ICAS 2012-0.4 |
General Lectures |
| BOMBARDIER
C-SERIES AIRCRAFT DEVELOPMENT |
ICAS 2012-0.5 |
General Lectures |
| VOLCANIC, WEATHER AND
CLIMATE EFFECTS ON AIR TRANSPORT |
ICAS 2012-0.6 |
General Lectures |
| MANAGING DIFFUSE ERUPTION
CLOUDS - THE EXPERIENCES OF 2010-11, AND THE RESULTS OF THE INTERNATIONAL
VOLCANIC ASH TASK FORCE |
ICAS 2012-0.7 |
General Lectures |
| HIFIRE: AN INTERNATIONAL COLLABORATION TO ADVANCE THE SCIENCE AND TECHNOLOGY OF HYPERSONIC FLIGHT |
ICAS 2012-0.8 |
General Lectures |
| A KNOWLEDGE BASED APPROACH
FOR EXTENDED PHYSICS-BASED WING MASS ESTIMATION IN EARLY DESIGN STAGES |
ICAS 2012-1.1.1 |
1. Aircraft and Systems
Integration |
| RECYCLING OLD WEIGHT
ASSESSMENT METHODS AND GIVING THEM NEW LIFE IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2012-1.1.2 |
1. Aircraft and Systems
Integration |
| METHODS FOR EVALUATION OF
AIRCRAFT MASS DISTRIBUTION |
ICAS 2012-1.1.3 |
1. Aircraft and Systems
Integration |
| 21ST CENTURY CHALLENGES FOR
THE DESIGN OF PASSENGER AIRCRAFT |
ICAS 2012-1.10.1 |
1. Aircraft and Systems
Integration |
| INVESTIGATION OF A
STRUT-BRACED WING CONFIGURATION FOR FUTURE COMMERCIAL TRANSPORT |
ICAS 2012-1.10.2 |
1. Aircraft and Systems
Integration |
| METHODOLOGY FOR A
PRELIMINARY DESIGN STUDY OF A BOX-WING AIRLINER |
ICAS 2012-1.10.3 |
1. Aircraft and Systems
Integration |
| CONCEPTUAL DESIGN AND AERODYNAMIC STUDY OF JOINED-WING
BUSINESS JET AIRCRAFT |
ICAS 2012-1.10.4 |
1. Aircraft and Systems
Integration |
| NOVEL LOW-FLYING
PROPELLER-DRIVEN AIRCRAFT CONCEPT FOR REDUCED DIRECT OPERATING COSTS AND
EMISSIONS |
ICAS 2012-1.10.5 |
1. Aircraft and Systems
Integration |
| THE AUSTRALIAN ARMY AND
UNMANNED AERIAL VEHICLES… 2O YEARS AND FINALLY IN-SERVICE |
ICAS 2012-1.11.1 |
1. Aircraft and Systems
Integration |
| EOLE, AN INNOVATIVE FLYING
SCALE DEMONSTRATOR FOR AIR-LAUNCH-TO-ORBIT AUTOMATIC SYSTEMS |
ICAS 2012-1.11.2 |
1. Aircraft and Systems
Integration |
| DESIGN AND CONFIGURATION
LAYOUTS OF AN ADVANCED LONG ENDURANCE UAV- LESSONS LEARNT AFTER FLIGHT
TESTING |
ICAS 2012-1.11.3 |
1. Aircraft and Systems
Integration |
| D-SEND PROJECT FOR LOW SONIC
BOOM DESIGN TECHNOLOGY |
ICAS 2012-1.2.1 |
1. Aircraft and Systems
Integration |
| DEVELOPMENT OF A SMALL-SCALE
SUPERSONIC FLIGHT EXPERIMENT VEHICLE AS A FLYING TEST BED |
ICAS 2012-1.2.2 |
1. Aircraft and Systems
Integration |
| CONCEPTUAL DESIGN STUDY ON
LOW BOOM LH2 SUPERSONIC TRANSPORT -
CONSIDERING CLIMATE CHANGE IMPACT |
ICAS 2012-1.2.3 |
1. Aircraft and Systems
Integration |
| DESIGN METHODS FOR AN
UNCONVENTIONAL SPLIT WING AIRCRAFT CONFIGURATION |
ICAS 2012-1.3.1 |
1. Aircraft and Systems
Integration |
| MODULAR AEROPLANE SYSTEM. A
CONCEPT AND INITIAL INVESTIGATION |
ICAS 2012-1.3.2 |
1. Aircraft and Systems
Integration |
| FANWING -- DEVELOPMENTS AND
APPLICATIONS |
ICAS 2012-1.3.3 |
1. Aircraft and Systems
Integration |
| MODELLING OF A WARPING WING
FOR ENERGY CONSUMPTION MINIMIZATION |
ICAS 2012-1.3.4 |
1. Aircraft and Systems
Integration |
| OPTIMISATION OF THE
HELICOPTER FUSELAGE WITH SIMULATION OF MAIN AND TAIL ROTOR INFLUENCE |
ICAS 2012-1.4.1 |
1. Aircraft and Systems
Integration |
| RESEARCH AND DEVELOPMENT OF
DOUBLE TETRAHEDRON HEXA-ROTORCRAFT (DOT-HR) |
ICAS 2012-1.4.2 |
1. Aircraft and Systems
Integration |
| INVESTIGATION OF LOW THRUST
TO WEIGHT RATIO ROTATIONAL CAPACITY OF ASYMMETRIC MONO-WING CONFIGURATIONS |
ICAS 2012-1.4.3 |
1. Aircraft and Systems
Integration |
| ASSESSING
HELICOPTER SURVIVABILITY TO GROUND LAUNCHED PROJECTILES USING MULTI-FIDELITY
INVERSE SIMULATION |
ICAS 2012-1.4.4 |
1. Aircraft and Systems
Integration |
| CONTROL-ORIENTED MODELING
AND ANALYSIS OF AERO-THERMO-ELASTIC-PROPULSION HYPERSONIC VEHICLE |
ICAS 2012-1.5.1 |
1. Aircraft and Systems
Integration |
| ADVANCED AEROSPACE SYSTEMS
WITH INTERCONTINENTAL AND GLOBAL RANGE OF FLIGHT |
ICAS 2012-1.5.2 |
1. Aircraft and Systems
Integration |
| DESIGN OF MASS SAVING
CONFIGURATIONS FOR WINGED REENTRY VEHICLES |
ICAS 2012-1.5.3 |
1. Aircraft and Systems
Integration |
| PARAMETRIC AIRCRAFT
CONCEPTUAL DESIGN SPACE |
ICAS 2012-1.6.1 |
1. Aircraft and Systems
Integration |
| AERODYNAMIC ANALYSIS AND
DESIGN OF A TWIN-ENGINE COMMUTER
AIRCRAFT |
ICAS 2012-1.6.2 |
1. Aircraft and Systems
Integration |
| HOW A HIGH-SCHOOL STUDENT
BUILT THE FIRST DUTCH HUMAN POWERED AIRCRAFT |
ICAS 2012-1.6.3 |
1. Aircraft and Systems
Integration |
| AIRCRAFT CONCEPTUAL DESIGN
IN A MULTI-LEVEL, MULTI-FIDELITY, MULTI-DISCIPLINARY OPTIMIZATION PROCESS |
ICAS 2012-1.6.4 |
1. Aircraft and Systems
Integration |
| THE EREA VISION ON HIGH
PRIORITY RESEARCH AXES TOWARDS AIR TRANSPORT SYSTEM 2050 |
ICAS 2012-1.7.1 |
1. Aircraft and Systems
Integration |
| A CONCEPTUAL DESIGN AND
ANALYSIS TOOL FOR BLENDED WING BODY AIRCRAFT |
ICAS 2012-1.7.2 |
1. Aircraft and Systems
Integration |
| DESIGNING PRO-COMPOSITE
AIRCRAFT CONCEPTS AND LAYOUTS TO MAXIMIZE POTENTIAL BENEFITS OF HIGH SPECIFIC
STRENGTH OF CFRP |
ICAS 2012-1.7.3 |
1. Aircraft and Systems
Integration |
| MISSION AND ECONOMIC
ANALYSIS OF AIRCRAFT WITH NATURAL LAMINAR FLOW TECHNOLOGY |
ICAS 2012-1.7.4 |
1. Aircraft and Systems
Integration |
| MULTI-DISCIPLINARY DESIGN
AND FEASIBILITY STUDY OF DISTRIBUTED PROPULSION SYSTEMS |
ICAS 2012-1.7.5 |
1. Aircraft and Systems
Integration |
| A HIGHLY EXPANDABLE LOW-COST
OPEN-SOURCE UAV SYSTEM WITH HIGH ON-BOARD PROCESSING POWER |
ICAS 2012-1.8.1 |
1. Aircraft and Systems
Integration |
| PRELIMINARY DESIGN OF A
FUEL-CELL-BASED HYBRID-ELECTRICAL UAV |
ICAS 2012-1.8.2 |
1. Aircraft and Systems
Integration |
| DESIGN AND TEST OF A UAV
BLENDED WING BODY CONFIGURATION |
ICAS 2012-1.8.3 |
1. Aircraft and Systems
Integration |
| COMMUNICATION IN AIRCRAFT
DESIGN: CAN WE ESTABLISH A COMMON LANGUAGE? |
ICAS 2012-1.9.1 |
1. Aircraft and Systems
Integration |
| TECHNOLOGY ASSESSMENT OF
FUTURE AIRCRAFT: SOCIO-ECO-EFFICIENCY IN CONCEPTUAL AIRCRAFT DESIGN |
ICAS 2012-1.9.2 |
1. Aircraft and Systems
Integration |
| AIRCRAFT SYSTEM SIMULATION
FOR PRELIMINARY DESIGN |
ICAS 2012-1.9.3 |
1. Aircraft and Systems
Integration |
| MADO – SOFTWARE PACKAGE FOR
HIGH ORDER MULTIDISCIPLINARY AIRCRAFT
DESIGN AND OPTIMIZATION |
ICAS 2012-1.9.4 |
1. Aircraft and Systems
Integration |
| SIMULTANEOUS OPTIMIZATION OF
AIRFRAME AND ENGINE FOR SUPERSONIC TRANSPORT |
ICAS 2012-12.3.4 |
1. Aircraft and Systems
Integration |
| THE WORKFLOW CONSTRUCTION
AND MANAGEMENT IN AERONAUTICAL MULTIDISCIPLINARY OPTIMIZATION |
ICAS 2012-2.1.2 |
1. Aircraft and Systems
Integration |
| ADVANCE SEAPLANE CONCEPTUAL
DESIGN ADAPTING TRIMARAN BOAT HULL CONCEPT |
ICAS 2012-2.1.3 |
1. Aircraft and Systems
Integration |
| VERY-LONG ENDURANCE SOLAR
POWERED AUTONOMOUS UAVS: ROLE AND CONSTRAINTS FOR GMES APPLICATIONS |
ICAS 2012-4.7.5 |
1. Aircraft and Systems
Integration |
| CARRIER SUITABILITY OF
LAND-BASED AIRCRAFT |
ICAS2012-1.1ST: |
1. Aircraft and Systems
Integration |
| AN INTEGRATED FRAMEWORK FOR
INNOVATIVE COMPOUND GYROPLANE DESIGN SYSTEM |
ICAS2012-1.4ST: |
1. Aircraft and Systems
Integration |
| THE INFLUENCE OF DEMOISELLE
AIRCRAFT ON LIGHT AND GENERAL AVIATION DESIGN |
ICAS2012-1.7ST: |
1. Aircraft and Systems
Integration |
| UAS DESIGN REQUIREMENTS FOR
OPERATION IN COLOMBIAN MOUNTAIN ENVIRONMENTS |
ICAS2012-1.8ST: |
1. Aircraft and Systems
Integration |
| BOX WING AIRCRAFT CONCEPTUAL
DESIGN |
ICAS2012-1.9ST: |
1. Aircraft and Systems
Integration |
| MULTIDISCIPLINARY EVALUATION
OF TRUSS-BRACED WING FOR FUTURE GREEN AIRCRAFT |
ICAS2012-1.10ST: |
1. Aircraft and Systems
Integration |
| FIRE-X
407 DEVELOPMENT: UNMANNING THE BELL HELICOPTER 407 WITH THE US NAVY FIRE
SCOUT MQ-8B AUTONOMOUS SYSTEM |
ICAS2012-P1.1 |
1. Aircraft and Systems
Integration |
| THE METHOD FOR NONLINEAR
ANALYSIS OPTIMIZATION IN AERONAUTICAL RESEARCH |
ICAS2012-P1.2 |
1. Aircraft and Systems
Integration |
| TETHERING
UNMANNED ROTORCRAFT FOR HIGH-ENDURANCE OPERATIONS |
ICAS2012-P1.3 |
1. Aircraft and Systems
Integration |
| UNMANNED MEASUREMENT
PLATFORM FOR PARAGLIDERS |
ICAS2012-P1.4 |
1. Aircraft and Systems
Integration |
| A FULLY AUTOMATED CAD-BASED
FRAMEWORK FOR SHAPE OPTIMIZATION |
ICAS 2012-11.10.1 |
2. Aerodynamics |
| GLOBAL OPTIMIZATION OF
TWO-DIMENSIONAL HIGH LIFT AERODYNAMIC SYSTEM |
ICAS 2012-11.10.2 |
2. Aerodynamics |
| ROBUST AERODYNAMIC DESIGN
OPTIMISATION OF MORPHING AEROFOIL/WING USING DISTRIBUTED MOGA |
ICAS 2012-11.10.3 |
2. Aerodynamics |
| IMPROVED PARTICLE SWARM
OPTIMIZATION BASED ON SOCIAL MODEL FOR AERODYNAMIC DESIGN |
ICAS 2012-11.10.4 |
2. Aerodynamics |
| WING-BODY OPTIMIZATION BASED
ON MULTI-FIDELITY SURROGATE MODEL |
ICAS 2012-11.10.5 |
2. Aerodynamics |
| THE ONERA ELSA CFD SOFTWARE
: INPUT FROM RESEARCH AND FEEDBACK FROM INDUSTRY |
ICAS 2012-2.1.1 |
2. Aerodynamics |
| AUTOMATIC HANDLING OF
DEFECTIVE SURFACE GEOMETRY WITHIN GRID GENERATION FOR NAVIER-STOKES
COMPUTATION |
ICAS 2012-2.11.1 |
2. Aerodynamics |
| SMALL DISTURBANCE
NAVIER-STOKES INVESTIGATIONS OF FIGHTER-TYPE-DELTA-WING PITCHING OSCILLATIONS |
ICAS 2012-2.11.2 |
2. Aerodynamics |
| RECENT DEVELOPMENTS TO THE
VISCOUS GARABEDIAN AND KORN METHOD |
ICAS 2012-2.11.3 |
2. Aerodynamics |
| DEVELOPMENT OF SUPERSONIC
NATURAL LAMINAR FLOW WING DESIGN SYSTEM USING CFD-BASED INVERSE METHOD |
ICAS 2012-2.2.1 |
2. Aerodynamics |
| DESIGN OF LAMINAR
SUPERCRITICAL AIRFOILS BASED ON NAVIER-STOKES EQUATIONS |
ICAS 2012-2.2.2 |
2. Aerodynamics |
| LAMINAR FLOW WING’S
OPTIMIZATION DESIGN BY RANS SOLVER WITH AUTOMATIC TRANSITION PREDICTION |
ICAS 2012-2.2.3 |
2. Aerodynamics |
| ON THE EFFECTS OF TURBULENCE
MODELING AND GRID REFINEMENT ON HIGH-LIFT CONFIGURATION AERODYNAMIC
SIMULATIONS |
ICAS 2012-2.3.1 |
2. Aerodynamics |
| NUMERICAL INVESTIGATION OF
FLOW OVER MULTI-ELEMENT AIRFOILS WITH LIFT-ENHANCING TABS |
ICAS 2012-2.3.2 |
2. Aerodynamics |
| NUMERICAL RESEARCH OF THE
NACELLE STRAKE ON A CIVIL JET |
ICAS 2012-2.3.3 |
2. Aerodynamics |
| MULTI-OBJECTIVE OPTIMIZATION
OF MULTI-ELEMENT HIGH-LIFT AIRFOIL |
ICAS 2012-2.3.4 |
2. Aerodynamics |
| BEYOND TWO-EQUATION
TURBULENCE MODELING FOR THE REYNOLDS-AVERAGED NAVIER-STOKES EQUATIONS:
ADVANCES IN COMPLEX FLOW PREDICTIONS |
ICAS 2012-2.4.1 |
2. Aerodynamics |
| NUMERICAL SIMULATION OF
THREE-DIMENSIONAL SHOCK-WAVE/BOUNDARY-LAYER INTERACTION ON SHARP AND BLUNTED
FLAT PLATE |
ICAS 2012-2.4.2 |
2. Aerodynamics |
| APPLICATION
OF TWO TRANSITION MODELS TO FLOWS AROUND AIRFOILS |
ICAS 2012-2.4.4 |
2. Aerodynamics |
| NUMERICAL STUDY ON THE
EFFECT OF VARYING SPANWISE TWIST ON LOW-REYNOLDS-NUMBER FLAPPING FLIGHT |
ICAS 2012-2.5.1 |
2. Aerodynamics |
| NUMERICAL STUDY OF PITCHING
OSCILLATION EFFECT ON AERODYNAMIC CHARACTERISTICS OVER ASYMMETRIC VORTEX
STRUCTURE OF SLENDER REVOLUTION |
ICAS 2012-2.5.2 |
2. Aerodynamics |
| NUMERICAL METHOD FOR ICE
ACCRETION ON 3D WINGS |
ICAS 2012-2.6.1 |
2. Aerodynamics |
| THE PERFORMANCE COMPUTATION
OF THE HOT AIR ANTI-ICING SYSTEM OF AN AERO-ENGINE CONE |
ICAS 2012-2.6.2 |
2. Aerodynamics |
| NUMERICAL SIMULATIONS OF
SELF-SUSTAINED AEROELASTIC OSCILLATIONS AT LOW REYNOLDS NUMBERS |
ICAS 2012-2.6.3 |
2. Aerodynamics |
| TRANSONIC FLUTTER, SHOCKS,
AND PARAMETER EFFECTS |
ICAS 2012-2.6.4 |
2. Aerodynamics |
| CFD BASED AEROELASTIC
CALCULATION OF PROPELLER LOADS |
ICAS 2012-9.8.1 |
2. Aerodynamics |
| TIME-ACCURATE VERSUS
ACTUATOR DISK SIMULATIONS OF PROPELLER SLIPSTREAM FLOWS |
ICAS 2012-9.8.2 |
2. Aerodynamics |
| EXPLORING
THE AERODYNAMIC INTERFERENCE OF PROPELLER-WING ON A SOLAR POWERED UNMANNED
AERIAL VEHICLE |
ICAS 2012-9.8.3 |
2. Aerodynamics |
| FLEXIBILITY OF AN ORITHOPTER
WING TESTED IN A WIND-TUNNEL |
ICAS 2012-12.5.3 |
2. Aerodynamics |
| RESULTS OF THE GUST
RESISTANT MAV PROGRAMME |
ICAS 2012-3.1.1 |
2. Aerodynamics |
| AERODYNAMIC MODEL OF
TRANSPORT AIRPLANE IN EXTENDED ENVELOPE FOR SIMULATION OF UPSET RECOVERY |
ICAS 2012-3.1.2 |
2. Aerodynamics |
| WATER TUNNEL FORCE AND
MOMENT STUDIES OF A MANEUVERING UCAV 1303 AND THEIR CONTROL |
ICAS 2012-3.1.3 |
2. Aerodynamics |
| SUBSONIC WAKE FLOWS ANALYSIS
BY DIGITAL THREE-WAVELENGTHS HOLOGRAPHIC INTERFEROMETRY |
ICAS 2012-3.11.3 |
2. Aerodynamics |
| STUDIES ON IMPROVEMENT OF
NONLINEAR PITCHING MOMENT CHARACTERISTICS OF CRANKED-ARROW WING |
ICAS 2012-3.2.1 |
2. Aerodynamics |
| A TECHNIQUE TO PREDICT THE
AERODYNAMIC LOSSES OF BATTLE DAMAGED WINGS |
ICAS 2012-3.2.2 |
2. Aerodynamics |
| TRAILING EDGE TREATMENT TO
ENHANCE HIGH LIFT SYSTEM PERFORMANCE |
ICAS 2012-3.2.3 |
2. Aerodynamics |
| FLEXIBLE WING AERODYNAMICS
AT LOW REYNOLDS NUMBERS |
ICAS 2012-3.3.1 |
2. Aerodynamics |
| THE INFLUENCE OF TURBULENCE
INTENSITY ON THE FLOW STRUCTURE OVER A THIN AIRFOIL AT LOW REYNOLDS NUMBERS |
ICAS 2012-3.3.2 |
2. Aerodynamics |
| OPTIMUM LOCATION OF PRESSURE
MEASUREMENTS AROUND A WING AS A DYNAMIC CONTROL INPUT IN SMOOTH AND TURBULENT
CONDITIONS |
ICAS 2012-3.3.3 |
2. Aerodynamics |
| EXPERIMENTAL INVESTIGATION
OF A BI-PLANE MICRO AIR VEHICLE |
ICAS 2012-3.3.4 |
2. Aerodynamics |
| APPLICATION OF DYNAMIC
PRESSURE MEASUREMENT FOR EMPENNAGE BUFFET |
ICAS 2012-3.4.1 |
2. Aerodynamics |
| BOUNDARY LAYER TRANSITION
DETECTION USING TEMPERATURE SENSITIVE PAINT IN THE ARA TRANSONIC WIND TUNNEL |
ICAS 2012-3.4.2 |
2. Aerodynamics |
| COMPARATIVE EVALUATION OF
ICING ON AERODYNAMIC SURFACES |
ICAS 2012-3.4.3 |
2. Aerodynamics |
| LABORATORY TESTING OF INSECT
CONTAMINATION FOR LAMINAR FLOW APPLICATIONS USING AN INSECT-IMPACT TEST
FACILITY |
ICAS 2012-3.4.4 |
2. Aerodynamics |
| AN EXPERIMENTAL STUDY OF A
PULSED AIR JET AND AN ACOUSTIC SYNTHETIC JET ON A LOW SPEED TURBULENT
BOUNDARY LAYER |
ICAS 2012-3.5.1 |
2. Aerodynamics |
| EXPERIMENTAL STUDIES ON
MICRO-VORTEX GENERATORS IN HYPERSONIC FLOW |
ICAS 2012-3.5.2 |
2. Aerodynamics |
| ACTIVE
SEPARATION CONTROL ON A 2D HIGH-LIFT WING SECTION TOWARDS HIGH REYNOLDS
NUMBER APPLICATION |
ICAS 2012-3.5.3 |
2. Aerodynamics |
| EXPERIMENTAL INVESTIGATION
OF FLAT PLATE SELF-NOISE REDUCTION USING TRAILING EDGE SERRATIONS |
ICAS 2012-9.11.1 |
2. Aerodynamics |
| WIND TUNNEL TESTING OF
POROUS DEVICES FOR THE REDUCTION OF FLAP SIDE-EDGE NOISE |
ICAS 2012-9.11.2 |
2. Aerodynamics |
| EXPERIMENTAL STUDY OF THE
MORPHING FLAP AS A LOW NOISE HIGH LIFT DEVICE FOR AIRCRAFT WING |
ICAS 2012-9.11.3 |
2. Aerodynamics |
| THERMAL NON-EQUILIBRIUM
EFFECTS IN RADICAL FARMING SCRAMJETS |
ICAS 2012-11.4.1 |
2. Aerodynamics |
| INSTABILITY CHARACTERISTICS
OF SHOCK WAVES AHEAD OF A HEMISPHERICAL SHELL AT SUPERSONIC SPEEDS |
ICAS 2012-11.4.2 |
2. Aerodynamics |
| STUDY ON THE FLOW STRUCTURES
OF THE SHOCKWAVE AND TURBULENT BOUNDARY-LAYER INTERACTION |
ICAS 2012-11.4.3 |
2. Aerodynamics |
| AN
APPROXIMATE ENGINEERING METHOD FOR AERODYNAMIC HEATING SOLUTION AROUND BLUNT
BODY NOES |
ICAS 2012-11.4.4 |
2. Aerodynamics |
| INFLUENCE OF TURBULENCE
SCALE AND SHAPE OF LEADING EDGE ON FST-INDUCED LAMINAR-TURBULENT TRANSITION |
ICAS 2012-2.4.3 |
2. Aerodynamics |
| STABILITY ANALYSIS ON
NATURAL LAMINAR FLOW WING IN SUPERSONIC FLOW: ONERA-JAXA JOINT RESEARCH
PROGRAM |
ICAS 2012-3.10.1 |
2. Aerodynamics |
| STREAMWISE AND CROSSFLOW
INSTABILITIES ON INCLINED CIRCULAR CYLINDERS |
ICAS 2012-3.10.2 |
2. Aerodynamics |
| HIFIRE-1 BOUNDARY-LAYER
TRANSITION MEASUREMENTS |
ICAS 2012-3.10.3 |
2. Aerodynamics |
| ON THE EFFECT OF DISTRIBUTED
ROUGHNESS ON TRANSITION OVER ROTOR-STATOR DEVICES |
ICAS 2012-3.10.4 |
2. Aerodynamics |
| MEASUREMENTS AND PREDICTION
OF LAMINAR-TURBULENT TRANSITION AT HIGH FREE-STREAM TURBULENCE & PRESSURE
GRADIENTS |
ICAS 2012-3.10.5 |
2. Aerodynamics |
| AIRFOIL SELF NOISE REDUCTION
BY APPLICATION OF DIFFERENT TYPES OF TRAILING EDGE SERRATIONS |
ICAS 2012-3.11.1 |
2. Aerodynamics |
| A COMPUTATIONAL STUDY OF THE
AERODYNAMICS OF A SPINNING CYLINDER IN CROSSFLOW OF HIGH REYNOLDS NUMBER |
ICAS 2012-3.11.2 |
2. Aerodynamics |
| ARTIFICIAL HINGED-WING
BIRD WITH ACTIVE TORSION AND PARTIALLY
LINEAR KINEMATICS |
ICAS 2012-3.6.1 |
2. Aerodynamics |
| HELICOPTER RETREATING BLADE
STALL CONTROL USING SELF-SUPPLYING AIR JET VORTEX |
ICAS 2012-3.6.2 |
2. Aerodynamics |
| AERODYNAMIC OPTIMISATION OF
A MORPHING MEMBRANE WING |
ICAS 2012-3.6.3 |
2. Aerodynamics |
| VORTEX FLOW MANIPULATION ON
GENERIC DELTA WING CONFIGURATIONS |
ICAS 2012-3.6.4 |
2. Aerodynamics |
| TIME DEPENDENT ANALYSIS OF A
RECTANGULAR SYNTHETIC JET |
ICAS 2012-3.7.1 |
2. Aerodynamics |
| NOVEL PASSIVE AND ACTIVE
FLOW CONTROL FOR HIGH LIFT |
ICAS 2012-3.7.2 |
2. Aerodynamics |
| FLOW CONTROL USING DBD
PLASMA ON BACKWARD-FACING STEP |
ICAS 2012-3.7.3 |
2. Aerodynamics |
| COMPUTATIONAL STUDY OF A
COMPARISON OF CO-FLOW AND COUNTER BLOWING DBD PLASMA ACTUATOR FOR SEPARATION
CONTROL OVER AN AIRFOIL |
ICAS 2012-3.7.4 |
2. Aerodynamics |
| EXPERIMENTAL/NUMERICAL
INVESTIGATION AIRFOIL WITH FLOW CONTROL BY SYNTHETIC JETS |
ICAS 2012-3.7.5 |
2. Aerodynamics |
| AEROTHERMODYNAMIC FIELD PAST
A REENTRY CAPSULE FOR SAMPLE RETURN MISSIONS |
ICAS 2012-3.8.1 |
2. Aerodynamics |
| MODELING OF THE INTERACTION
BETWEEN A TURBULENT FLOW AND AN ABLATABLE MATERIAL |
ICAS 2012-3.8.2 |
2. Aerodynamics |
| STUDY OF RADIATIVE HEAT
TRANSFER IN TITAN ATMOSPHERIC ENTRY |
ICAS 2012-3.8.3 |
2. Aerodynamics |
| AEROACOUSTIC ANALYSIS OF A
HELICOPTER CONFIGURATION WITH DUCTED TAIL ROTOR |
ICAS 2012-3.9.1 |
2. Aerodynamics |
| ESTIMATION OF NOISE
SHIELDING EFFECT OF NEXT-GENERATION AIRCRAFT BY A COMPUTATIONAL AEROACOUSTICS
METHOD |
ICAS 2012-3.9.2 |
2. Aerodynamics |
| COMPUTATIONAL STUDY ON NOISE
GENERATION FROM A TWO-WHEEL MAIN LANDING GEAR |
ICAS 2012-3.9.3 |
2. Aerodynamics |
| STUDY ON NOISE OF COUNTER
ROTATING FAN MODELS AT CIAM ANECHOIC CHAMBER |
ICAS 2012-3.9.4 |
2. Aerodynamics |
| SWISS / FINNISH
COMPUTATIONAL FLUID DYNAMICS SIMULATION ON THE F/A-18 |
ICAS 2012-10.6.1 |
2. Aerodynamics |
| EXTERNAL AERODYNAMIC
PRESSURE LOADS FOR A RIGID FIGHTER AIRCRAFT, A COMPARISON BETWEEN PSP AND CFD |
ICAS 2012-10.6.2 |
2. Aerodynamics |
| PROGRESS IN UNDERSTANDING
TRANSONIC AND SUPERSONIC GROUND EFFECT AERODYNAMICS |
ICAS 2012-10.6.3 |
2. Aerodynamics |
| A RECENT HISTORY OF THE
EVOLUTION OF AUSTRALIA’S AERODYNAMICS STORE SEPARATION CAPABILITY – THROUGH
INDIGENOUS AND INTERNATIONAL PROGRAMS |
ICAS 2012-10.6.4 |
2. Aerodynamics |
| AUTOMATED CHAIN FOR
AERODYNAMIC COMPUTATIONS MEETING AIRCRAFT TRIMMING REQUIREMENTS |
ICAS 2012-2.10.1 |
2. Aerodynamics |
| NUMERICAL STUDY OF THE
REYNOLDS NUMBER EFFECT ON LOW ASPECT
RATIO WINGS AT LOW SPEED |
ICAS 2012-2.10.2 |
2. Aerodynamics |
| THE INVESTIGATION OF A
POSSIBILITY OF INCREASING THE LIFT-TO-DRAG RATIO OF A MANEUVERABLE AIRCRAFT
AT SUBSONIC SPEEDS |
ICAS 2012-2.10.3 |
2. Aerodynamics |
| ACTIVE
CONTROL OF SHOCK/BOUNDARY LAYER INTERACTION FOR TRANSONIC DRAG REDUCTION OF
AIRFOILS |
ICAS 2012-2.10.4 |
2. Aerodynamics |
| INVESTIGATION
ON PROPELLER ENGINE OPTIMUM INSTALLATION POSITION ON A SOLAR POWERED UNMANNED
AERIAL VEHICLE |
ICAS 2012-2.10.5 |
2. Aerodynamics |
| COMPUTATIONAL AND
EXPERIMENTAL ANALYSIS OF THE ACTIVE MORPHING WING CONCEPT |
ICAS 2012-2.5.3 |
2. Aerodynamics |
| AERODYNAMICS ANALYSIS OF
CYCLOIDAL ROTOR |
ICAS 2012-2.7.1 |
2. Aerodynamics |
| NUMERICAL AND EXPERIMENTAL
ANALYSIS OF A REPRESENTATIVE ADF HELICOPTER FUSELAGE |
ICAS 2012-2.7.2 |
2. Aerodynamics |
| FLOW CHARACTERISTICS OF A
HELICOPTER FUSELAGE CONFIGURATION INCLUDING A ROTATING ROTOR HEAD |
ICAS 2012-2.7.3 |
2. Aerodynamics |
| PERFORMANCE ANALYSIS OF A
COAXIAL ROTOR SYSTEM IN HOVER: THREE POINTS OF VIEW |
ICAS 2012-2.7.4 |
2. Aerodynamics |
| INFLUENCE OF FLAPPING WING
UNSTEADY MOTION ON AERODYNAMIC PERFORMANCE OF HORIZONTAL TAIL |
ICAS 2012-2.7.5 |
2. Aerodynamics |
| NUMERICAL INVESTIGATION ON
THE POTENTIAL OF STEAM COOLING FOR THE SKYLON SPACEPLANE IN HYPERSONIC FLOW |
ICAS 2012-2.8.1 |
2. Aerodynamics |
| ELLIPTICALLY CONICAL TWIST
AND CAMBER OF DELTA WINGS |
ICAS 2012-2.8.2 |
2. Aerodynamics |
| AN EXPERIMENTAL AND
NUMERICAL STUDY OF THE EFFECT OF NOSE BLUNTING ON A CONICAL NOSED BODY AT
TRANSONIC SPEED |
ICAS 2012-2.8.3 |
2. Aerodynamics |
| RESEARCH FOR JET FLOW INFLUENCES TO WING-MOUNTED CIVIL
AIRCRAFT AERODYNAMIC CHARACTERISTICS |
ICAS 2012-2.9.1 |
2. Aerodynamics |
| CONCEPTUAL DESIGN AND
AERODYNAMIC STUDY OF BLENDED WING BODY BUSINESS JET |
ICAS 2012-2.9.2 |
2. Aerodynamics |
| AN EXPERIENCE IN AERODYNAMIC
DESIGN OF TRANSPORT AIRCRAFT |
ICAS 2012-2.9.3 |
2. Aerodynamics |
| EXPERIMENTAL AND NUMERICAL
INVESTIGATIONS OF LOCAL AERODYNAMICS OF CIVIL AIRCRAFT |
ICAS 2012-2.9.4 |
2. Aerodynamics |
| HIGH-LIFT SYSTEMS FOR
ENHANCED TAKEOFF PERFORMANCE |
ICAS 2012-9.5.1 |
2. Aerodynamics |
| AERODYNAMICS OF STOL
AIRPLANES WITH POWERED HIGH-LIFT SYSTEMS |
ICAS 2012-9.5.2 |
2. Aerodynamics |
| INVESTIGATION ON STRUCTURAL
AND AERODYNAMIC CHARACTERISTICS OF RESONANT TYPE ELASTIC FLAPPING WING |
ICAS 2012-9.5.3 |
2. Aerodynamics |
| A COMPUTATIONAL STUDY ON THE
DESIGN OF AIRFOILS FOR A FIXED WING MAV AND THE AERODYNAMIC CHARACTERISTIC OF
THE VEHICLE |
ICAS2012-2.2ST: |
2. Aerodynamics |
| MULTI-OBJECTIVE AERODYNAMIC
OPTIMIZATION DESIGN OF MULTI-ELEMENT AIRFOIL USING KRIGING MODEL |
ICAS2012-2.3ST: |
2. Aerodynamics |
| CHARACTERISTICS
OF AN 80-DEG SWEPT DELTA WING IN WING ROCK OR FREE YAWING |
ICAS2012-3.1ST1: |
2. Aerodynamics |
| MULTI-DEGREE-OF-FREEDOM
DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
ICAS2012-3.1ST2: |
2. Aerodynamics |
| STEADY
AND UNSTEADY FLOWS PAST AIRFOILS AT LOW REYNOLDS NUMBERS IN THE PROXIMITY OF
THE GROUND |
ICAS2012-3.6ST: |
2. Aerodynamics |
| SIMULATION OF THE FULL
COUPLING BETWEEN THE RADIATION TRANSFER AND THE AERODYNAMICS FOR HYPERSONIC REENTRY PROBES |
ICAS2012-3.8ST: |
2. Aerodynamics |
| A LEAP
IN LEARNED BIO-INSPIRED FLIGHT |
ICAS2012-9.5ST: |
2. Aerodynamics |
| AERODYNAMIC
ANALYSIS OF 3-D FLAPPING WING MOTION VIA THE HILBERT-HUANG TRANSFORM METHOD |
ICAS2012-9.8ST: |
2. Aerodynamics |
| WIND TUNNEL AND CFD STUDY OF
AIRFOIL WITH AIRBRAKE |
ICAS2012-10.6ST1: |
2. Aerodynamics |
| NON-LINEAR BEHAVIOUR OF A
WING DUE TO UNDERWING STORES |
ICAS2012-10.6ST2: |
2. Aerodynamics |
| EXTENSIONS OF MENTER’S SST
TRANSITION MODEL TO SIMULATE HYPERSONIC AND CROSS-FLOW TRANSITION |
ICAS2012-11.4ST: |
2. Aerodynamics |
| DEVELOPMENT OF FAST
UNSTRUCTURED CFD CODE “FASTAR” |
ICAS2012-2.11ST: |
2. Aerodynamics |
| DYNAMIC SURFACE PRESSURE
MEASUREMENTS ON A FLAPPING WING IN SMOOTH AND TURBULENT FLOW |
ICAS2012-9.11ST1: |
2. Aerodynamics |
| COMPARISON OF INFILL
SAMPLING CRITERIA IN KRIGING-BASED AERODYNAMIC OPTIMIZATION |
ICAS2012-11.10ST: |
2. Aerodynamics |
| NUMERICAL RESEARCH OF THE
AIR INTAKE LOCATION INFLUENCE ONTO THE HIGH-SPEED AIRCRAFT PERFORMANCE |
ICAS2012-P2.1 |
2. Aerodynamics |
| THE
INTEGRATION OPTIMIZATION DESIGN OF AERODYNAMIC AND STEALTH FOR FIGHTERS |
ICAS2012-P2.2 |
2. Aerodynamics |
| TRANSONIC
DRAG REDUCTION ON A SUPERCRITICAL WING SECTION USING SHOCK CONTROL BUMPS |
ICAS2012-P2.3 |
2. Aerodynamics |
| NUMERICAL SIMULATION OF
TRANSONIC SHOCK-VORTEX INTERACTION FLOW AROUND THE VFE-2 DELTA WING BASED ON
MDDES |
ICAS2012-P2.4 |
2. Aerodynamics |
| FLOW
CONTROL TEST RESEARCH OF AIRCRAFT MODEL WITH ADJUSTABLE CANAEDS |
ICAS2012-P2.5 |
2. Aerodynamics |
| AN EXPERIENCE OF USING
NUMERICAL METHODS IN EXPERIMENTAL INVESTIGATIONS OF TsAGI |
ICAS2012-P2.6 |
2. Aerodynamics |
| INVESTIGATION OF PASSIVE
FLOW CONTROL METHODOLOGIES USING SST-IDDES |
ICAS2012-P2.7 |
2. Aerodynamics |
| ON SOUND GENERATION BY
MOVING SURFACES AND CONVECTED SOURCES IN A FLOW |
ICAS2012-P2.8 |
2. Aerodynamics |
| THE STUDY ON THE AIRCRAFT
INTEGRATED CHARACTERS WITH DIFFERENT HEIGHT WINGLETS |
ICAS2012-P2.9 |
2. Aerodynamics |
| EXPERIMENTAL INVESTIGATIONS
OF HYDRAULIC DEVICES PERFORMANCE IN AVIATION ENGINE COMPARTMENT |
ICAS2012-P2.10 |
2. Aerodynamics |
| THEORETICAL AND EXPERIMENTAL
INVESTIGATIONS ON CHOKING PHENOMENA OF AXISYMMETRIC CONVERGENT NOZZLE FLOW |
ICAS2012-P2.11 |
2. Aerodynamics |
| STABILIZING EFFECT OF
LONGITUDINAL-WALL OSCILLATION ON 2D CHANNEL FLOW |
ICAS2012-P2.12 |
2. Aerodynamics |
| PRELIMINARY AERODYNAMIC
INVESTIGATION OF AN UNMANNED BOX-WING AIRCRAFT |
ICAS2012-P2.13 |
2. Aerodynamics |
| A PRELIMINARY CFD
INVESTIGATION ON REAR FUSELAGE SUPPORT CORRECTION |
ICAS2012-P2.14 |
2. Aerodynamics |
| OPTIMIZATION OF
TWO-DIMENSIONAL WING IN GROUND EFFECT CONSIDERING AERODYNAMIC CENTRE OF
HEIGHT AND LIFT |
ICAS2012-P2.15 |
2. Aerodynamics |
| CFD-BASED RESEARCH OF STRAKE
EFFECTS FOR LOW SPEED HIGH LIFT CONFIGURATION |
ICAS2012-P2.16 |
2. Aerodynamics |
| ANALYSIS
OF FLUCTUATING LOAD OF A CIRCULAR CYLINDER UNDER THE FUSELAGE |
ICAS2012-P2.17 |
2. Aerodynamics |
| MANEUVERABILITY OF AN UAV
WITH COANDA EFFECT BASED LIFT PRODUCTION |
ICAS2012-P2.18 |
2. Aerodynamics |
| COMPUTATIONAL INVESTIGATION
OF ICING CONTAMINATION ON AIRFOIL |
ICAS2012-P2.19 |
2. Aerodynamics |
| EVALUATION OF DYNAMIC
BEHAVIOR OF A DEPLOYABLE WING UAV BY DROP TEST |
ICAS2012-P2.20 |
2. Aerodynamics |
| ENERGY SUPPLY EFFECT ON
SUPERSONIC BOUNDARY LAYER RECEPTIVITY AND STABILITY |
ICAS2012-P2.21 |
2. Aerodynamics |
| AERODYNAMIC CHARACTERISTICS
OF A BIRD-LIKE ASSEMBLED WING |
ICAS2012-P2.22 |
2. Aerodynamics |
| CFD COMPUTATION OF THE
GROUND EFFECT ON AIRPLANE WITH HIGH ASPECT RATIO WING |
ICAS2012-P2.23 |
2. Aerodynamics |
| A NEW APPROACH TO IDENTIFICATION AND OPTIMIZATION OF AIRFOILS
BY USING THE COMBINATORIAL-CYCLIC METHOD |
ICAS2012-P2.24 |
2. Aerodynamics |
| MICROSTRUCTURE AND
MECHANICAL PROPERTIES OF LASER CLADDING REPAIR OF AISI 4340 STEEL |
ICAS 2012-12.4.4 |
3. Materials and Structures |
| ANALYSIS OF MULTIPLE SITE
DAMAGE IN AIRCRAFT STRUCTURES BY USING WEIGHT FUNCTION METHOD IN FRACTURE
MECHANICS |
ICAS 2012-7.1.1 |
3. Materials and Structures |
| STRENGTH CRITERIA
DEVELOPMENT FOR COMPOSITE STRUCTURES BASING ON SOLUTIONS SUPERPOSITION FOR
MODELS OF DIFFERENT LEVELS |
ICAS 2012-7.1.2 |
3. Materials and Structures |
| RESEARCH ON CRACK GROWTH OF
MULTIPLE-SITE DAMAGED STRUCTURE |
ICAS 2012-7.1.3 |
3. Materials and Structures |
| DIARC PLASMA COATING FOR
RELIABLE AND DURABLE STRUCTURAL BONDING OF METALS |
ICAS 2012-7.2.1 |
3. Materials and Structures |
| SPD REPAIRS TO THIN
ALUMINIUM STRUCTURES |
ICAS 2012-7.2.2 |
3. Materials and Structures |
| FINITE ELEMENT SIMULATION OF
CRACK PROPAGATION IN MILITARY AIRCRAFT COATINGS |
ICAS 2012-7.2.3 |
3. Materials and Structures |
| NUMERICAL STUDY ON RESIDUAL
THERMAL STRESSES IN CARBON FIBRE PULLOUT |
ICAS 2012-7.3.1 |
3. Materials and Structures |
| AN INVESTIGATION OF MODE I
FRACTURE TOUGHNESS USING ALIGNED CARBON-NANOTUBE FORESTS AT THE CRACK
INTERFACE |
ICAS 2012-7.3.2 |
3. Materials and Structures |
| LCF BEHAVIOR AND LIFE
EVALUATION OF A SINGLE CRYSTAL NICKEL BASE SUPERALLOY UNDER DIFFERENT DWELL
CONDITION |
ICAS 2012-7.3.3 |
3. Materials and Structures |
| EFFECT OF LATERAL PLACEMENT
OF CERAMIC AND METAL GRAINS ON THERMAL STRESS DISTRIBUTION THROUGHOUT FGMS |
ICAS 2012-7.3.4 |
3. Materials and Structures |
| THE DETERMINATION OF
DELAMINATION STRAIN ENERGY RELEASE RATE OF COMPOSITE BI-MATERIAL INTERFACE |
ICAS 2012-7.4.1 |
3. Materials and Structures |
| NUMERICAL SIMULATIONS AND
EXPERIMENTAL INVESTIGATIONS ON QUASI-STATIC AND CYCLIC MIXED MODE
DELAMINATION OF MULTIDIRECTIONAL CFRP LAMINATES |
ICAS 2012-7.4.2 |
3. Materials and Structures |
| SIZE EFFECT OF FAILURE MODES
IN COMPOSITE LAMINATES UNDER COMPRESSION |
ICAS 2012-7.4.3 |
3. Materials and Structures |
| POST-BUCKLING
BEHAVIOR OF LAMINATED STRINGER STIFFENED PANEL UNDER COMPRESSIVE
LOAD—EXPERIMENTS AND ANALYSIS |
ICAS 2012-7.4.4 |
3. Materials and Structures |
| TITANIUM METAL MATRIX
COMPOSITE DEVELOPMENT FOR COMMERCIAL AIRCRAFT LANDING GEAR STRUCTURE |
ICAS 2012-7.5.1 |
3. Materials and Structures |
| DAMAGE TOLERANCE OF Z-PINNED
COMPOSITE JOINTS |
ICAS 2012-7.5.2 |
3. Materials and Structures |
| A COMPOSITE AND
METAL JOINT FOR A PROPELLER BLADE ROOT |
ICAS 2012-7.5.3 |
3. Materials and Structures |
| REPAIR CONCEPT SUPPORTED BY
LASER REMOVAL AND INDUCTIVE HEATING |
ICAS 2012-7.6.1 |
3. Materials and Structures |
| DELAMINATION TOUGHENING OF
CARBON-EPOXY LAMINATE WITH A POLYETHYLENE-CO-METHACRYLIC ACID (EMAA)
SELF-HEALING MODIFIER |
ICAS 2012-7.6.2 |
3. Materials and Structures |
| MANUFACTURING
OF COMPOSITE AIRFRAME STRUCTURE BY RESIN TRANSFER MOLDING PROCESS |
ICAS 2012-7.6.3 |
3. Materials and Structures |
| EVALUATION ON DISCRETE
SOURCE DAMAGES OF CFRP STIFFENED PANELS |
ICAS 2012-7.7.1 |
3. Materials and Structures |
| ENERGY DISTRIBUTION IN GLARE
AND 2024-T3 ALUMINIUM DURING LOW-VELOCITY IMPACT |
ICAS 2012-7.7.2 |
3. Materials and Structures |
| THE DYNAMIC BEHAVIOR OF
FUNCTIONALLY GRADED PLATES UNDER THE IMPACT LOADING |
ICAS 2012-7.7.3 |
3. Materials and Structures |
| CRACK NUCLEATION MODELING IN
NOTCHED SPECIMEN SUBJECTED TO HIGH FATIGUE LOADING |
ICAS 2012-7.7.4 |
3. Materials and Structures |
| COUPLED
MICROMECHANICS-FINITE ELEMENT PROGRESSIVE FAILURE DYNAMIC ANALYSIS APPROACH:
F-16 CANOPY CASE STUDY |
ICAS 2012-7.7.5 |
3. Materials and Structures |
| DIRECTIONAL ENHANCEMENT OF
COMPOSITE STRUCTURES ENERGY ABSORPTION USING MAGNETORHEOLOGICAL FLUIDS |
ICAS 2012-7.8.1 |
3. Materials and Structures |
| INTERFACE DIFFUSION AND
MORPHOLOGY OF AEROSPACE GRADE EPOXY CO-CURED WITH THERMOPLASTIC POLYMERS |
ICAS 2012-7.8.2 |
3. Materials and Structures |
| ANALYTICAL INVESTIGATIONS ON
LIGHT-WEIGHT STRUCTURES FOR SATELLITE STRUCTURAL FRAME APPLICATIONS THROUGH
3D MODELING |
ICAS 2012-7.8.3 |
3. Materials and Structures |
| INVESTIGATION OF AN
IN-SERVICE CRACK SUBJECTED TO AERODYNAMIC BUFFET AND MANOEUVRE LOADS AND
EXPOSED TO AN CORROSIVE ENVIRONMENT |
ICAS 2012-7.9.1 |
3. Materials and Structures |
| INVESTIGATION OF CRACK
PROPAGATION BY OPTICAL INTERFEROMETRIC MEASUREMENTS OF LOCAL DEFORMATION
RESPONSE |
ICAS 2012-7.9.2 |
3. Materials and Structures |
| PROBABILISTIC RISK ANALYSIS
FOR AIRCRAFT STRUCTURES WITH LIMITED IN-SERVICE DAMAGES |
ICAS 2012-7.9.3 |
3. Materials and Structures |
| STRUCTURAL
INTEGRITY ANALYSIS AND TEST OF FATIGUE CRITICAL LOCATION OF MA60 REGIONAL JET |
ICAS 2012-7.9.4 |
3. Materials and Structures |
| AEROELASTIC ANALYSIS FOR
HELICOPTER ROTOR BLADES IN HOVER AND FORWARD FLIGHTS |
ICAS 2012-11.5.3 |
3. Materials and Structures |
| EXPERIMENTAL AND NUMERICAL
ASSESSMENT OF HELICOPTER SUBFLOOR CRASHWORTHINESS |
ICAS 2012-8.1.1 |
3. Materials and Structures |
| IMPROVED DESIGN METHODS FOR
CRASHWORTHY COMPOSITE HELICOPTER STRUCTURES |
ICAS 2012-8.1.2 |
3. Materials and Structures |
| POSTBUCKLING COMPUTATION OF
LARGE STIFFENED STRUCTURES |
ICAS 2012-8.1.3 |
3. Materials and Structures |
| NEOCASS: AN OPEN SOURCE
ENVIRONMENT FOR THE AEROELASTIC ANALYSIS AT CONCEPTUAL DESIGN LEVEL |
ICAS 2012-8.10.1 |
3. Materials and Structures |
| NUMERICAL SIMULATION OF
SHOCK-STALL FLUTTER OF A HIGH-ASPECT-RATIO FORWARD-SWEPT WING |
ICAS 2012-8.10.2 |
3. Materials and Structures |
| VIBRATION AND AEROELASTIC CLEARANCE WORK FOR JASSM INTEGRATION ONTO THE F/A-18A/B |
ICAS 2012-8.10.3 |
3. Materials and Structures |
| ANALYSIS OF STATIC AND
DYNAMIC AEROELASTIC CHARACTERISTICS OF AIRPLANE IN TRANSONIC FLOW |
ICAS 2012-8.10.4 |
3. Materials and Structures |
| FLOW-INDUCED FLUTTER OF
SLENDER CANTILEVER HIGH-COMPLIANCE PLATES |
ICAS 2012-8.10.5 |
3. Materials and Structures |
| THE INSTABILITY OF THE
PIPELINE DUE TO TRANSPORTING FLUID’S PRESSURE RIPPLES |
ICAS 2012-8.11.1 |
3. Materials and Structures |
| REAL
TIME DIAGNOSIS OF DYNAMIC FAILURE IN FUTURE AEROSPACE STRUCTURES |
ICAS 2012-8.11.2 |
3. Materials and Structures |
| APPLICATION
OF SINGULAR VALUE DECOMPOSITION IN COMPONENT MODE SYNTHESIS WITH EXPERIMENTAL
APPROACH |
ICAS 2012-8.11.3 |
3. Materials and Structures |
| IMPROVED EXACT STRIP
POSTBUCKLING ANALYSIS FOR ANISOTROPIC PLATES WITH FIXED, FREE AND STRAIGHT
EDGES |
ICAS 2012-8.2.1 |
3. Materials and Structures |
| SEMI-ANALYTICAL SPRING-IN
ANALYSIS TO COUNTERACT CFRP MANUFACTURING DEFORMATIONS BY TOOL COMPENSATION |
ICAS 2012-8.2.2 |
3. Materials and Structures |
| MAKING THE INVISIBLE
VISIBLE: JOINING THE DOTS FROM LORD KELVIN TO FIGHTER JET FATIGUE |
ICAS 2012-8.2.3 |
3. Materials and Structures |
| PRELIMINARY INVESTIGATION ON
THE FEASIBILITY OF A BIRD SURROGATE FOR FULL-SCALE BIRD IMPACT TEST |
ICAS 2012-8.3.1 |
3. Materials and Structures |
| IDENTIFICATION OF HELICOPTER
GROUND RESONANCE WITH MULTI-BODY SIMULATION |
ICAS 2012-8.3.2 |
3. Materials and Structures |
| MODELLING OF IMPACT ON
SANDWICH STRUCTURE FOR FAST MAINTENANCE LOOPS |
ICAS 2012-8.3.3 |
3. Materials and Structures |
| COMPOSITE SANDWICH PANEL
BIRDSTRIKE TESTING AND ANALYSIS |
ICAS 2012-8.3.4 |
3. Materials and Structures |
| DESIGN CONSIDERATIONS OF A
PRESSURE DRIVEN MORPHING WING STRUCTURE |
ICAS 2012-8.4.1 |
3. Materials and Structures |
| DEVELOPMENT OF GEODESIC
COMPOSITE AIRCRAFT STRUCTURES |
ICAS 2012-8.4.2 |
3. Materials and Structures |
| DESIGN AND AERO-ELASTIC
OPTIMISATION OF THE STRUCTURE OF THE LAPCAT A2 MACH 5 AIRLINER |
ICAS 2012-8.4.3 |
3. Materials and Structures |
| DESIGN OF COMPOSITE
STRUCTURES FOR IMPROVED AEROELASTIC PERFORMANCE |
ICAS 2012-8.4.4 |
3. Materials and Structures |
| AEROELASTIC SIMULATION OF
FLEXIBLE FLAPPING WING BASED ON STRUCTURAL FEM AND QUASI-STEADY AERODYNAMIC
MODEL |
ICAS 2012-8.5.1 |
3. Materials and Structures |
| THE EXTENSION OF
DISCRETE-TIME FLUTTER MARGIN |
ICAS 2012-8.5.2 |
3. Materials and Structures |
| AEROELASTIC RESPONSE OF A
CHORDWISE FLEXIBLE WINGS SUBJECTED TO GUSTS: AN INITIAL STUDY ON EXPERIMENTAL
AND COMPUTATIONAL VALIDATION |
ICAS 2012-8.5.3 |
3. Materials and Structures |
| NONLINEAR AEROELASTIC
ANALYSIS OF SWEPT WINGS IN COMPRESSIBLE FLOW VIA THE HARMONIC BALANCE METHOD |
ICAS 2012-8.7.1 |
3. Materials and Structures |
| A COUPLED AERO AND
STRUCTURAL DYNAMICS MODEL FOR COMPUTATION OF UNSTEADY LOADS ON THE HELICOPTER
SKELDAR V200 |
ICAS 2012-8.7.2 |
3. Materials and Structures |
| DESIGN AND VERIFICATION OF
FLUTTER SUPPRESSION CONTROL SYSTEMS BY MULTIDISCIPLINARY CO-SIMULATIONS |
ICAS 2012-8.7.3 |
3. Materials and Structures |
| AEROELASTIC
MULTIDISCIPLINARY ANALYSIS OF THE FIN
WITH INNOVATIVE ADAPTIVE CONTROL |
ICAS 2012-8.7.4 |
3. Materials and Structures |
| THE NEW OPTIMALITY CRITERIA
FOR STRUCTURAL DESIGN WITH CONSTRAINING ELASTIC DISPLACEMENTS |
ICAS 2012-8.7.5 |
3. Materials and Structures |
| DESIGN, DEVELOPMENT AND
MANUFACTURING OF THE ALCAS CFRP DOOR SURROUND STRUCTURE |
ICAS 2012-8.8.1 |
3. Materials and Structures |
| NOVEL APPROACH AND ALGORITHM
FOR SEARCHING RATIONAL NONCONVENTIONAL AIRFRAME CONCEPTS OF NEW GENERATION
AIRCRAFTS |
ICAS 2012-8.8.2 |
3. Materials and Structures |
| THE COMPREHENSIVE STUDY ON
ADVANCED WINGTIP DEVICES IN LARGE CIVIL AIRCRAFT |
ICAS 2012-8.8.3 |
3. Materials and Structures |
| ASSESSMENT OF STRUCTURAL
EFFECT OF SELECTIVE STITCHING ON COMPOSITE SKIN-STIFFENER BONDING |
ICAS 2012-8.9.1 |
3. Materials and Structures |
| APPLICATION
OF A SCALAR STRAIN-BASED DAMAGE ONSET THEORY TO THE FAILURE OF A COMPLEX
COMPOSITE SPECIMEN |
ICAS 2012-8.9.2 |
3. Materials and Structures |
| BUCKLING-OPTIMIZED VARIABLE
STIFFNESS LAMINATES FOR A COMPOSITE FUSELAGE WINDOW SECTION |
ICAS 2012-8.9.3 |
3. Materials and Structures |
| NUMERICAL
SIMULATION OF BIRD-STRIKING PROCESS AND ITS EXPERIMENTAL VERIFICATION |
ICAS 2012-8.9.4 |
3. Materials and Structures |
| LAY-UP OPTIMIZATION OF
COMPOSITE PLATES TO DELAY MODE-JUMP INSTABILITIES |
ICAS2012-7.1ST: |
3. Materials and Structures |
| THE FABRICATION AND
CHARACTERIZATION OF TiO2 UV DETECTOR |
ICAS2012-7.3ST: |
3. Materials and Structures |
| THE CFRP SAILPLANE WING
SEGMENTS MANUFACTURED BY FILAMENT PLACEMENT |
ICAS2012-7.5ST: |
3. Materials and Structures |
| ON THE
KNEE-POINT PHENOMENON IN COMPOSITE LAMINATES UNDER LOW-VELOCITY IMPACT AND
QUASI-STATIC INDENTATION |
ICAS2012-7.7ST: |
3. Materials and Structures |
| POST-BUCKLING
BEHAVIOR AND PROPAGATION OF DELAMINATION FOR COMPOSITE PANELS IN DIFFERENT
DELAMINATION SIZES |
ICAS2012-7.9ST: |
3. Materials and Structures |
| EXPERIMENTAL DEVELOPMENT AND
ANALYSIS OF AN ACTIVE CRUSHING ELEMENT USING PRESSURIZED COMPOSITE TUBES |
ICAS2012-8.1ST: |
3. Materials and Structures |
| ANALYTICAL METHOD FOR LIMIT
LOAD CAPACITY CALCULATION OF THIN WALLED AIRCRAFT STRUCTURES |
ICAS2012-8.2ST: |
3. Materials and Structures |
| COMPUTATIONAL AND
EXPERIMENTAL RESEARCH OF BOLT JOINTS OF METAL AND COMPOSITE IN AIRFRAMES |
ICAS2012-8.4ST: |
3. Materials and Structures |
| LOAD SYNTHESIS OF HELICOPTER
DYNAMIC COMPONENTS: IMPROVEMENTS TO LINEAR REGRESSION IN THE AZIMUTH DOMAIN |
ICAS2012-8.10ST: |
3. Materials and Structures |
| EIGENVALUE AND FLUTTER
SENSITIVITY ANALYSIS OF AIRLINER WING |
ICAS2012-P3.1 |
3. Materials and Structures |
| ANALYTICAL NATURAL
FREQUENCIES OF TAPERED WINGS |
ICAS2012-P3.2 |
3. Materials and Structures |
| INTERGRANULAR CORROSION
PROTOCOL DEVELOPMENT FOR 7075-T651 EXTRUSION |
ICAS2012-P3.3 |
3. Materials and Structures |
| INVESTIGATION INTO OPTIMISED
COMPOSITE SCARF REPAIRS WITH PRACTICAL CONSTRAINTS |
ICAS2012-P3.4 |
3. Materials and Structures |
| TOOL DEVELOPMENT FOR
AIRCRAFT LOADS POST-PROCESSING |
ICAS2012-P3.5 |
3. Materials and Structures |
| FINDING TUNING FREQUENCY OF
SYMMETRIC AND ANTI-SYMMETRIC LAMB WAVES USING FEM |
ICAS2012-P3.6 |
3. Materials and Structures |
| BUCKLING
AND POST-BUCKLING RESPONSES OF SQUARE LAMINATE WITH VARIOUS SHAPED CUTOUTS
UNDER DIFFERENT LOADINGS |
ICAS2012-P3.7 |
3. Materials and Structures |
| WAVELET-BASED ACTIVE SENSING
FOR QUANTITATIVE ASSESSMENT OF THROUGH-THICKNESS CRACK SIZE AND ANGLE IN
COMPOSITE PLATES |
ICAS2012-P3.8 |
3. Materials and Structures |
| VERIFICATION OF OPTICAL
PAYLOAD CFRP STRUCTURE FOR SATELLITE THROUGH ANALYSIS AND SPACE QUALIFICATION
TEST |
ICAS2012-P3.9 |
3. Materials and Structures |
| DEVELOPMENT OF AN
EXPERIMENTAL TECHNIQUE FOR HIGH TEMPERATURE IMPINGEMENT STUDIES |
ICAS 2012-12.6.3 |
4. Propulsion |
| VIBRATION STRENGTH INCREASE
OF ROTATING BLADES USING DYNAMIC SPIN RIGS |
ICAS 2012-12.6.4 |
4. Propulsion |
| ENERGY-BASED METHOD FOR GAS
TURBINE ENGINE DISK BURST SPEED CALCULATION |
ICAS 2012-4.1.1 |
4. Propulsion |
| PREVENTION OF LOW CYCLE
FATIGUE FRACTURE OF AVIATION ENGINE CRITICAL PARTS |
ICAS 2012-4.1.2 |
4. Propulsion |
| ACHIEVEMENT OF BIMETALLIC
BLISKS INTEGRATED DISSIMILAR ALLOYS FOR PROMISING HIGH TEMPERATURE AVIATION
GAS TURBINE ENGINES |
ICAS 2012-4.1.3 |
4. Propulsion |
| IMPROVED MODELLING OF
VORTICAL MIXING FOR THE SIMULATION OF EFFICIENT PROPULSION SYSTEMS |
ICAS 2012-4.10.1 |
4. Propulsion |
| HOT END TECHNOLOGY FOR
ADVANCED, LOW EMISSION LARGE CIVIL AIRCRAFT ENGINES |
ICAS 2012-4.10.2 |
4. Propulsion |
| PROPELLER INDUCED GROUND
VORTEX |
ICAS 2012-4.10.3 |
4. Propulsion |
| TURBOJET ANALYTICAL MODEL
DEVELOPMENT AND VALIDATION |
ICAS 2012-4.10.5 |
4. Propulsion |
| NUMERICAL MODELLING OF
POROUS FUEL INJECTION IN A RADICAL FARMING SCRAMJET |
ICAS 2012-4.11.1 |
4. Propulsion |
| JET INTERACTION IN A
HYPERSONIC FLOW: A COMPARISON BETWEEN PLIF THERMOMETRY AND COMPUTATIONAL
SIMULATION |
ICAS 2012-4.11.2 |
4. Propulsion |
| ROBUST DESIGN OPTIMIZATION
OF HIGH-PERFORMANCE AXISYMMETRIC SCRAMJETS BASED ON SURROGATE-ASSISTED
EVOLUTIONARY ALGORITHMS |
ICAS 2012-4.11.3 |
4. Propulsion |
| PREDICTION OF THE KINETICS
OF THE 3D STRESS-STRAIN STATE OF HIGH-TEMPERATURE GAS TURBINE BLADES WITH
LIMITED EXPERIMENTAL DATA |
ICAS 2012-4.2.1 |
4. Propulsion |
| ACCELERATED LIFE CONSUMPTION
DUE TO THERMO-ACOUSTIC OSCILLATIONS IN GAS TURBINES: XFEM & CRACK |
ICAS 2012-4.2.2 |
4. Propulsion |
| DETAILED POST-SOFT IMPACT
PROGRESSIVE DAMAGE ANALYSIS FOR A HYBRID STRUCTURE JET ENGINE |
ICAS 2012-4.2.3 |
4. Propulsion |
| EVALUATION OF A MULTIPLE
FREQUENCY PHASE LAGGED METHOD FOR UNSTEADY NUMERICAL SIMULATIONS OF
MULTISTAGE TURBOMACHINERY |
ICAS 2012-4.3.1 |
4. Propulsion |
| ROBUST LIFECYCLE
OPTIMIZATION OF TURBINE COMPONENTS USING SIMULATION PLATFORMS |
ICAS 2012-4.3.2 |
4. Propulsion |
| INTERDISCIPLINARY COMPLEX
DESIGN OF MODERN HIGH AND LOW PRESSURE TURBINES |
ICAS 2012-4.3.3 |
4. Propulsion |
| INTEGRATED DESIGN METHOD OF
A ROCKET ENGINE TURBOPUMP SUB-SYSTEM FOR SUPPRESSING ROTOR LATERAL VIBRATION |
ICAS 2012-4.3.4 |
4. Propulsion |
| THE EFFECT OF PLASMA
ACTUATORS ON TIP CLEARANCE FLOWS IN COMPRESSOR ROTORS |
ICAS 2012-4.4.1 |
4. Propulsion |
| EXPERIMENTAL AND NUMERICAL
RESEARCH OF UNSTEADY FLOW IN CURVILINEAR CHANNEL WITH ACTIVE FLOW MANAGEMENT
USING “SYNTHETIC” JETS |
ICAS 2012-4.4.2 |
4. Propulsion |
| THE
NUMERICAL SIMULATION OF BIRD STRIKE ON BLADES OF AN ENGINE |
ICAS 2012-4.4.3 |
4. Propulsion |
| TURB'OPTY-BASED OPTIMIZATION
OF A SHROUDED FAN WITH CASING TREATMENT |
ICAS 2012-4.4.4 |
4. Propulsion |
| DESIGN, SIMULATION AND
ANALYSIS OF A PARALLEL HYBRID-ELECTRIC PROPULSION SYSTEM FOR UNMANNED AERIAL
VEHICLES |
ICAS 2012-4.5.1 |
4. Propulsion |
| HARDWARE-IN-THE-LOOP
SIMULATION OF FUEL-CELL-BASED HYBRID-ELECTRICAL UAV PROPULSION |
ICAS 2012-4.5.2 |
4. Propulsion |
| AERODYNAMIC
DESIGN OF PROPELLER FOR LONG ENDURANCE |
ICAS 2012-4.5.3 |
4. Propulsion |
| EXPERIMENTAL AND NUMERICAL
STUDY OF TWO FIRST HIGHLY-LOADED STAGES OF COMPRESSORS AS A PART OF HPC AND
SEPARATE UNIT |
ICAS 2012-4.6.1 |
4. Propulsion |
| NUMERICAL INVESTIGATION OF
THE EFFECT OF INFLOW DISTORTIONS ON TRANSONIC AXIAL COMPRESSOR STAGES WITH 2D
AND 3D CALCULATIONS |
ICAS 2012-4.6.2 |
4. Propulsion |
| CFD OPTIMIZATION OF A
TRANSONIC COMPRESSOR USING MULTIOBJECTIVE GA AND METAMODELS |
ICAS 2012-4.6.3 |
4. Propulsion |
| DERIVATED TURBULENCE MODEL
TO PREDICT HARMONIC LOADS IN TRANSONIC SEPARATED FLOWS OVER A BUMP |
ICAS 2012-4.6.4 |
4. Propulsion |
| NUMERICAL TOOLS DEVELOPED AT
ONERA FOR THE AERODYNAMIC ASSESSMENT OF PROPELLERS AND COUNTER-ROTATING OPEN
ROTORS |
ICAS 2012-4.7.1 |
4. Propulsion |
| VOLTAIR - THE ALL ELECTRIC
PROPULSION CONCEPT PLATFORM – A VISION FOR ATMOSPHERIC FRIENDLY FLIGHT |
ICAS 2012-4.7.2 |
4. Propulsion |
| STUDIES
OF PROPULSION SYSTEM CONCEPTS FOR ADVANCED SUBSONIC AIRLINERS |
ICAS 2012-4.7.3 |
4. Propulsion |
| STUDIES ON REQUIRED
PERFORMANCES OF ADVANCED SUPERSONIC CIVIL AIRCRAFT AND THEIR PROPULSION
SYSTEMS FOR 2020-2035 TIMEFRAME |
ICAS 2012-4.7.4 |
4. Propulsion |
| PERFORMANCE TEST OF A
SMALL-SCALE TURBOJET ENGINE RUNNING ON A PALM OIL BIODIESEL - JET A BLEND |
ICAS 2012-4.8.1 |
4. Propulsion |
| TUNABLE DIODE LASER
ABSORPTION SPECTROSCOPY OF HYPERSONIC FLOWS |
ICAS 2012-4.8.2 |
4. Propulsion |
| EXPERIMENTAL STUDY OF
SUPERSONIC INLET FOR SUPPRESSION OF BUZZ IN SUBCRITICAL OPERATION |
ICAS 2012-6.2.1 |
4. Propulsion |
| PERFORMANCE EVALUATION OF A
BOUNDARY-LAYER DIVERTER FOR SUPERSONIC PROPULSION SYSTEM |
ICAS 2012-6.2.2 |
4. Propulsion |
| APPLICATION OF THE FAST
CALCULATION TECHNOLOGIES TO SIMULATION OF NON-STATIONARY SUPERSONIC VISCID
FLOW WITH COMBUSTION |
ICAS 2012-6.2.3 |
4. Propulsion |
| DESIGN ANALYSIS FOR HYBRID
PROPULSION |
ICAS 2012-6.7.5 |
4. Propulsion |
| ENGINEERING FAILURE MODES
AND FRACTURE CHARACTERISTICS OF SINGLE CRYSTAL SUPERALLOY BLADES |
ICAS2012-4.2ST: |
4. Propulsion |
| EFFECT ON THE AERODYNAMIC
FORCING IN AN AXIAL TURBINE STAGE ON VARYING STATOR BLADE SHAPE |
ICAS2012-4.3ST: |
4. Propulsion |
| STUDY OF THE PRESSURE DROP
FOR RADIAL INFLOW BETWEEN CO-ROTATING DISCS |
ICAS2012-4.4ST: |
4. Propulsion |
| COMPARISON OF PERFORMANCE OF
PROPELLER BLADES BY DIFFERENCE IN PLANAR SHAPE |
ICAS2012-4.6ST1: |
4. Propulsion |
| COMPUTATIONAL STUDY ON THE
INFLUENCE OF COANDA JET ON AIRFOILS: TWO-DIMENSIONAL CASE |
ICAS2012-4.6ST2: |
4. Propulsion |
| EXPERIMENTAL
INVESTIGATION OF INFRARED STEALTH TECHNOLOGIES OF AERO-ENGINE EXHAUST SYSTEM |
ICAS2012-P4.1 |
4. Propulsion |
| JET
NOISE REDUCTION BY MICROJETS |
ICAS2012-P4.2 |
4. Propulsion |
| INTAKE CAPABILITY
IMPROVEMENTS IN RAMJET-TYPE PROPULSION SYSTEM |
ICAS2012-P4.3 |
4. Propulsion |
| EFFECT OF VENT MIXER TO
MIXING CHARACTERISTICS IN SUPERSONIC FLOW |
ICAS2012-P4.4 |
4. Propulsion |
| VISUALIZATION OF UNSTEADY
BEHAVIOR OF SHOCK WAVES AROUND SUPERSONIC INTAKE INSTALLED IN SHOCK TUNNEL |
ICAS2012-P4.5 |
4. Propulsion |
| MODELING OF NO AND OH
INFRARED RADIATION ON A CONVERGENT-DIVERGENT NOZZLE |
ICAS2012-P4.6 |
4. Propulsion |
| FRACTURE
ANALYSIS OF BLADE DOVETAIL OF TC11 TITANIUM ALLOY |
ICAS2012-P4.7 |
4. Propulsion |
| DESIGN
OF A TWO-DIMENSIONAL GASDYNAMIC NOZZLE USING MULTI-OBJECTIVE PARTICLE SWARM
OPTIMISATION |
ICAS2012-P4.8 |
4. Propulsion |
| THERMAL ANALYSIS NEAR
SECONDARY INJECTION HOLE IN SITVC SYSTEM |
ICAS2012-P4.9 |
4. Propulsion |
| NUMERICAL MODELING OF FLOW
IN GASDYNAMIC RESONATOR AND MODEL VALIDATION BY RESULTS OF PULSE ENGINE TESTS |
ICAS2012-P4.10 |
4. Propulsion |
| PRE-STRESSED MODAL ANALYSIS
OF A TURBINE SPACER |
ICAS2012-P4.11 |
4. Propulsion |
| PERFORMANCE ANALYSIS OF A
SCRAMJET INLET-ISOLATOR USING EXPERIMENTAL & NUMERICAL METHODS |
ICAS2012-P4.12 |
4. Propulsion |
| OPTIMAL HIGH-SPEED
HELICOPTER TRANSMISSION DESIGNS |
ICAS2012-P4.13 |
4. Propulsion |
| FUEL CELLS ON ALTERNATIVE
NON – OIL FUELS FOR GAS TURBINE ENGINES OF AN ADVANCED CIVIL AIRCRAFTS |
ICAS2012-P4.14 |
4. Propulsion |
| THE EXPERIENCE OF HIGH
PRESSURE RATIO SINGLE STAGE HPT DESIGNING |
ICAS2012-P4.15 |
4. Propulsion |
| STREAMWISE PORTHOLE FUEL
INJECTION FOR BOUNDARY-LAYER COMBUSTION INSIDE A SCRAMJET ENGINE |
ICAS 2012-P4.16 |
4. Propulsion |
| FLIGHT TESTS OF TRANSPORT
AIRCRAFT UPSET RECOVERY TECHNIQUES AND THE SYSTEM OF INFORMATION SUPPORT OF
CREW |
ICAS 2012-5.1.1 |
5. Flight Dynamics and Control |
| FAULT DETECTION AND
RECONFIGURATION APPLIED TO A HELICOPTER SWASHPLATE ACTUATOR |
ICAS 2012-5.1.2 |
5. Flight Dynamics and Control |
| EMERGENCY PROPULSION-BASED
AUTOLAND SYSTEM |
ICAS 2012-5.1.3 |
5. Flight Dynamics and Control |
| NONLINEAR AERODYNAMIC
MODELING OF UNSTABLE AIRCRAFT USING FLIGHT TEST DATA |
ICAS 2012-5.10.1 |
5. Flight Dynamics and Control |
| MEASURING AND MODELLING THE
LONGITUDINAL MOTION OF PARAGLIDERS |
ICAS 2012-5.10.2 |
5. Flight Dynamics and Control |
| MODELING OF LOSS OF TAIL
ROTOR EFFECTIVENESS CONDUCTING TO UNANTICIPATED YAW |
ICAS 2012-5.10.3 |
5. Flight Dynamics and Control |
| REAL-TIME WAVELET FLIGHT
DATA EVALUATOR FOR SYSTEM IDENTIFICATION OF FLIGHT CHARACTERISTICS |
ICAS 2012-5.10.4 |
5. Flight Dynamics and Control |
| ESTIMATION OF AERODYNAMIC
DERIVATIVES IN AIRCRAFT MODEL USING ITERATIVE LEARNING IDENTIFICATION |
ICAS 2012-5.10.5 |
5. Flight Dynamics and Control |
| FLIGHT DEMONSTRATION OF
FAULT TOLERANT FLIGHT CONTROL SYSTEM |
ICAS 2012-5.2.1 |
5. Flight Dynamics and Control |
| DEVELOPMENT OF THE AUTOMATED
SYSTEM ON THE BASIS OF NEURAL NETWORKS FOR FLIGHT SAFETY OF AIRCRAFT |
ICAS 2012-5.2.2 |
5. Flight Dynamics and Control |
| ADAPTIVE CONTROL INVERSION
AND ACTUATOR FAILURE COMPENSATION FOR UAVS |
ICAS 2012-5.2.3 |
5. Flight Dynamics and Control |
| GUIDANCE AND CONTROL LAW FOR
D-SEND#2 |
ICAS 2012-5.3.1 |
5. Flight Dynamics and Control |
| RIDE CONTROL FOR THE
PERSONAL PLANE |
ICAS 2012-5.3.2 |
5. Flight Dynamics and Control |
| CONTROL ALLOCATION FOR
AIRCRAFTS WITH MULTIPLE CONTROL EFFECTORS DURING TAKEOFF AND LANDING PHASES |
ICAS 2012-5.3.3 |
5. Flight Dynamics and Control |
| AUTOPILOT
DESIGN FOR THE EOLE DEMONSTRATOR |
ICAS 2012-5.3.4 |
5. Flight Dynamics and Control |
| FLY-BY-WIRE AUGMENTED MANUAL
CONTROL - BASIC DESIGN CONSIDERATIONS |
ICAS 2012-5.4.1 |
5. Flight Dynamics and Control |
| AEROSERVOELASTIC FLIGHT CONTROL DESIGN FOR A MILITARY COMBAT AIRCRAFT WEAPON SYSTEM |
ICAS 2012-5.4.2 |
5. Flight Dynamics and Control |
| FLEXFOIL:
BIO-INSPIRED INTELLIGENT CONTROL ALGORITHM USING ARTIFICIAL NEURAL NETWORKS
FOR WING MORPHING |
ICAS 2012-5.4.3 |
5. Flight Dynamics and Control |
| THE SHEFEX II EXPERIMENTAL
RE-ENTRY VEHICLE: PRESENTATION OF FLIGHT TEST RESULTS |
ICAS 2012-5.4.4 |
5. Flight Dynamics and Control |
| ANALYTIC METHOD FOR FLIGHT
MOTION OF AIRCRAFT WITH A SINGLE VIDEO CAMERA AND ITS APPLICATION TO A FREE
FLIGHT GLIDER |
ICAS 2012-5.6.1 |
5. Flight Dynamics and Control |
| FLIGHT PERFORMANCE OF
LIGHTWEIGHT GYROPLANES |
ICAS 2012-5.6.2 |
5. Flight Dynamics and Control |
| METHODS AND FACILITIES TO BE
USED TO EVALUATE THE AIRCRAFT FLIGHT AND NAVIGATION EQUIPMENT IN FLIGHT TESTS |
ICAS 2012-5.6.3 |
5. Flight Dynamics and Control |
| RESEARCH ON OPTIMIZING
ASCENT TRAJECTORY OF AERO-SPACE PLANE BASED ON COMBINED CYCLE PROPULSION |
ICAS 2012-5.7.1 |
5. Flight Dynamics and Control |
| A GENERAL FOOTPRINT
GENERATION APPROACH FOR LIFTING RE-ENTRY VEHICLE |
ICAS 2012-5.7.2 |
5. Flight Dynamics and Control |
| ANGLE OF ATTACK OPERATION
ZONE ANALYSIS AND DESIGN FOR LIFTING ENTRY |
ICAS 2012-5.7.3 |
5. Flight Dynamics and Control |
| A PEG-BASED ASCENDING
GUIDANCE ALGORITHM FOR RAMJET-POWERED VEHICLES |
ICAS 2012-5.7.4 |
5. Flight Dynamics and Control |
| A NEW APPROACH FOR RE-ENTRY
VEHICLE TRAJECTORY PLANNING AND GUIDANCE |
ICAS 2012-5.7.5 |
5. Flight Dynamics and Control |
| OPERATIONAL
HUMAN-IN-THE-LOOP INTEGRATION OF 4D ARRIVAL GUIDANCE |
ICAS 2012-5.8.1 |
5. Flight Dynamics and Control |
| ENGINE-OUT TAKEOFF PATH
OPTIMIZATION OUT OF TERRAIN CHALLENGING AIRPORTS |
ICAS 2012-5.8.2 |
5. Flight Dynamics and Control |
| STATISTICAL STABILITY AND
CONTROL ANALYSIS TO INVESTIGATE THE CONTROL EFFORT OF IMPROVING HANDLING
QUALITY CHARACTERISTICS |
ICAS 2012-5.9.1 |
5. Flight Dynamics and Control |
| TECHNIQUE FOR FLYING
QUALITIES AND PIO PREDICTION |
ICAS 2012-5.9.2 |
5. Flight Dynamics and Control |
| EFFECTS OF MANIPULATOR TYPE
AND FEEL SYSTEM CHARACTERISTICS ON HIGH-FREQUENCY BIODYNAMIC PILOT-AIRCRAFT
INTERACTION |
ICAS 2012-5.9.3 |
5. Flight Dynamics and Control |
| SOME ASPECTS OF MOVING-BASE
SIMULATION OF UPSET RECOVERING MANEUVER |
ICAS 2012-5.9.4 |
5. Flight Dynamics and Control |
| MODEL VALIDATION OF A
TILTWING UAV IN TRANSITION PHASE APPLYING WINDTUNNEL INVESTIGATIONS |
ICAS 2012-11.1.1 |
5. Flight Dynamics and Control |
| CONTROL CONCEPT OF A
TILTWING UAV DURING LOW SPEED MANOEUVRING |
ICAS 2012-11.1.2 |
5. Flight Dynamics and Control |
| TRANSITION FLIGHT OF QUAD
TILT WING VTOL UAV |
ICAS 2012-11.1.3 |
5. Flight Dynamics and Control |
| FLIGHT TRIAL OF AN
ELECTRO-OPTICAL SENSE-AND-AVOID SYSTEM |
ICAS 2012-11.2.1 |
5. Flight Dynamics and Control |
| MULTIPLE UAV FORMATION
RECONFIGURATION WITH COLLISION AVOIDANCE GUIDANCE VIA DIFFERENTIAL GEOMETRY
CONCEPT |
ICAS 2012-11.2.2 |
5. Flight Dynamics and Control |
| DESCRIPTION AND EVALUATION
OF MULTI-THREAT TRACKING ARCHITECTURES |
ICAS 2012-11.2.3 |
5. Flight Dynamics and Control |
| VISUAL SERVOING APPROACH TO
COLLISION AVOIDANCE FOR AIRCRAFT |
ICAS 2012-11.3.1 |
5. Flight Dynamics and Control |
| VISION-BASED UAV GUIDANCE
AND ESTIMATION FOR AERIAL TARGET TRACKING |
ICAS 2012-11.3.2 |
5. Flight Dynamics and Control |
| GROUND-BASED SENSE AND AVOID
SUPPORT FOR UNMANNED AIRCRAFT SYSTEMS |
ICAS 2012-11.3.3 |
5. Flight Dynamics and Control |
| COLLISION AVOIDANCE OF
INDOOR FLYING DOUBLE TETRAHEDRON HEXA-ROTORCRAFT |
ICAS 2012-11.5.1 |
5. Flight Dynamics and Control |
| DESIGN OF A mu SYNTHESIS
CONTROLLER TO STABILIZE AN UNMANNED HELICOPTER |
ICAS 2012-11.5.2 |
5. Flight Dynamics and Control |
| ALL-SOURCE NAVIGATION FOR
ENHANCING UAV OPERATIONS IN GPS-DENIED ENVIRONMENTS |
ICAS 2012-11.6.1 |
5. Flight Dynamics and Control |
| INTELLIGENT LANDING SYSTEM
FOR LANDING UAVS AT UNSURVEYED AIRFIELDS |
ICAS 2012-11.6.2 |
5. Flight Dynamics and Control |
| EXTENDING AUTONOMY
CAPABILITIES FOR UNMANNED SYSTEMS WITH CRUSER |
ICAS 2012-11.6.3 |
5. Flight Dynamics and Control |
| OPTIMIZATION OF A NEW
MULTI-PURPOSE UAS FOR SCIENTIFIC APPLICATIONS USING AERODYNAMIC
RECONFIGURATION |
ICAS 2012-11.6.4 |
5. Flight Dynamics and Control |
| AN INNOVATIVE MISSION
MANAGEMENT SYSTEM FOR FIXED-WING UAVS |
ICAS 2012-11.7.1 |
5. Flight Dynamics and Control |
| REAL TIME PATH PLANNING
METHOD OF AIRCRAFT FORMATIONS |
ICAS 2012-11.7.2 |
5. Flight Dynamics and Control |
| HYBRID GAME EVOLUTIONARY
ALGORITHM FOR MISSION PATH PLANNING OF AERIAL SURVEY TASKS |
ICAS 2012-11.7.3 |
5. Flight Dynamics and Control |
| INFORMATION THEORY APPLIED
TO A SELF-ORGANISED, UNMANNED AERIAL SYSTEM |
ICAS 2012-11.7.4 |
5. Flight Dynamics and Control |
| CONTROLLER DESIGN AND
ANALYSIS OF UNMANNED AERIAL VEHICLES USING AUTOMATIC GAIN GENERATION
TECHNIQUE |
ICAS 2012-11.8.1 |
5. Flight Dynamics and Control |
| HIGH ANGLE OF ATTACK FLIGHT
CONTROL OF A TAIL-SITTER UNMANNED AIRCRAFT |
ICAS 2012-11.8.2 |
5. Flight Dynamics and Control |
| EXTRACTING DECK TREND TO
PLAN DESCENT TRAJECTORY FOR SAFE LANDING OF UAVS |
ICAS 2012-11.8.3 |
5. Flight Dynamics and Control |
| DEVELOPMENT OF NAVIGATION
ALGORITHMS FOR NAP-OF-THE-EARTH UAV FLIGHT IN A CONSTRAINED URBAN ENVIRONMENT |
ICAS 2012-11.9.1 |
5. Flight Dynamics and Control |
| THE FLAPPING AIRCRAFT
DYNAMICS WITH WING DEFORMATION UNDER GUST INPUT |
ICAS 2012-11.9.2 |
5. Flight Dynamics and Control |
| DESIGN OF ROBUST FLIGHT
CONTROL SYSTEM FOR SMALL FIXED-WING UAV |
ICAS 2012-11.9.3 |
5. Flight Dynamics and Control |
| DEVELOPMENT OF POSE
ESTIMATION SYSTEM BASED ON DUAL CAMERA TECHNIQUES FOR PARAMETER
IDENTIFICATION OF INDOOR MAV |
ICAS 2012-11.9.4 |
5. Flight Dynamics and Control |
| STUDY ON
MODELING PILOT BEHAVIOR BY ARTIFICIAL NEURAL NETWORK |
ICAS2012-5.9ST: |
5. Flight Dynamics and Control |
| A GREY-BOX SYSTEM
IDENTIFICATION PROCEDURE FOR SCALE MODEL HELICOPTERS BASED ON
FREQUENCY-DOMAIN ESTIMATION METHODS |
ICAS2012-11.9ST: |
5. Flight Dynamics and Control |
| RESEARCH ON METHODS OF
DYNAMIC MODELING AND SIMULATION FOR MORPHING WING AIRCRAFT |
ICAS2012-5.10ST: |
5. Flight Dynamics and Control |
| MODEL FOLLOWING TOTAL IN
FLIGHT SIMULATOR AS AN EDUCATIONAL TOOL |
ICAS2012-P5.1 |
5. Flight Dynamics and Control |
| MANEUVERING TARGET TRACKING
BASED ON THE EKF |
ICAS2012-P5.2 |
5. Flight Dynamics and Control |
| A MODEL OF HORIZONTAL
TAILPLANE DAMAGE FOR USE IN FLIGHT DYNAMICS |
ICAS2012-P5.3 |
5. Flight Dynamics and Control |
| AUTOPILOT DESIGN FOR AN
AGILE MISSILE USING L1 ADAPTIVE BACKSTEPPING CONTROL |
ICAS2012-P5.4 |
5. Flight Dynamics and Control |
| UAV COLLISION AVOIDANCE VIA
OPTIMAL TRAJECTORY GENERATION METHOD |
ICAS2012-P5.5 |
5. Flight Dynamics and Control |
| BI-OBJECTIVE PSEUDOSPECTRAL
OPTIMAL CONTROL TECHNIQUES FOR AIRCRAFT TRAJECTORY OPTIMIZATION |
ICAS2012-P5.6 |
5. Flight Dynamics and Control |
| TERRAIN REFERENCED UAV
NAVIGATION WITH LIDAR - A COMPARISON OF SEQUENTIAL PROCESSING AND BATCH
PROCESSING ALGORITHMS |
ICAS2012-P5.7 |
5. Flight Dynamics and Control |
| FORMATION SHAPE CONTROL OF
UNMANNED AIR VEHICLES |
ICAS2012-P5.8 |
5. Flight Dynamics and Control |
| GUST RESPONSE ANALYSIS IN
THE FLIGHT FORMATION OF UNMANNED AIR VEHICLES |
ICAS2012-P5.9 |
5. Flight Dynamics and Control |
| DEVELOPMENT OF OBSERVATIONAL
SYSTEM WITH UNMANNED FLIGHT SYSTEM |
ICAS2012-P5.10 |
5. Flight Dynamics and Control |
| STABILIZATION OF
LONGITUDINAL AIRCRAFT MOTION USING MODEL PREDICTIVE CONTROL AND EXACT
LINEARIZATION |
ICAS2012-P5.11 |
5. Flight Dynamics and Control |
| FUZZY LOGIC BASED FLIGHT
CONTROL SYSTEM FOR THE NIGERIAN AIR FORCE AIR BEETLE AIRCRAFT |
ICAS2012-P5.12 |
5. Flight Dynamics and Control |
| RESEARCH ON FAILURE
SIMULATION OF CIVIL AIRCRAFT FLIGHT MANAGEMENT SYSTEM |
ICAS 2012-5.6.4 |
6. Systems, Subsystems and
Equipment |
| CARGO FIRE PROTECTION
SYSTEMS FOR FREIGHTER CONVERSIONS |
ICAS 2012-6.10.1 |
6. Systems, Subsystems and
Equipment |
| EVALUATION OF CABIN
DISPLACEMENT VENTILATION UNDER FLIGHT CONDITIONS |
ICAS 2012-6.10.2 |
6. Systems, Subsystems and
Equipment |
| RESEARCH ON AIRBORNE
INTELLIGENT HYDRAULIC PUMP SYSTEM |
ICAS 2012-6.10.3 |
6. Systems, Subsystems and
Equipment |
| MULTIDISCIPLINARY DESIGN AND
FLIGHT TESTING OF A REMOTE GAS/PARTICLE AIRBORNE SENSOR SYSTEM |
ICAS 2012-6.10.4 |
6. Systems, Subsystems and
Equipment |
| ACOUSTIC
POWER AND DATA FOR MORE ROBUST FLIGHT DATA AND COCKPIT VOICE RECORDERS |
ICAS 2012-6.10.5 |
6. Systems, Subsystems and
Equipment |
| DESIGN STUDY OF AN ACTIVE
GURNEY FLAP SYSTEM FOR HELICOPTER ROTOR BLADES |
ICAS 2012-6.11.1 |
6. Systems, Subsystems and
Equipment |
| WEIGHT ON WHEEL SYSTEM BASED
ON STRAIN GAUGES |
ICAS 2012-6.11.2 |
6. Systems, Subsystems and
Equipment |
| A COMPUTER WITH OPERATIONAL
REDUNDANCY AND INTEGRATED ONBOARD NETWORKING AS BASE FOR AVIONICS OF ZERO
MAINTENANCE EQUIPMENT |
ICAS 2012-6.11.3 |
6. Systems, Subsystems and
Equipment |
| INNOVATIVE
MOISTURE/ICING-RESISTANT FLUSH AIR DATA SYSTEM |
ICAS 2012-6.5.1 |
6. Systems, Subsystems and
Equipment |
| COLD FUEL TEST RIG TO
INVESTIGATE ICE ACCRETION ON DIFFERENT PUMP INLET FILTER-MESH SCREENS |
ICAS 2012-6.5.2 |
6. Systems, Subsystems and
Equipment |
| COUPLING MECH. & THERMAL
MODELS IN PRELIMINARY DESIGN OF POWER TRANSMISSIONS DRIVEN BY THERMAL ISSUES |
ICAS 2012-6.6.1 |
6. Systems, Subsystems and
Equipment |
| MODELING OF FLUID CONDITION
OF AIRCRAFT HYDRAULIC SYSTEM |
ICAS 2012-6.6.2 |
6. Systems, Subsystems and
Equipment |
| A METHOD FOR THE EVALUATION
OF ELECTROMECHANICAL ACTUATOR SYSTEMS USING EXERGY |
ICAS 2012-6.6.3 |
6. Systems, Subsystems and
Equipment |
| MORE ELECTRICAL
ENVIRONMENTAL CONTROL SYSTEM SIMULATION |
ICAS 2012-6.6.4 |
6. Systems, Subsystems and
Equipment |
| BI-AXIAL VIBRATION ENERGY
HARVESTING FOR USE ON AEROSPACE PLATFORMS |
ICAS 2012-6.7.1 |
6. Systems, Subsystems and
Equipment |
| MORE/ALL ELECTRIC AIRCRAFT
BASED ON FUEL CELL ENERGY SYSTEM: THE ENFICA-FC EXPERIENCE |
ICAS 2012-6.7.2 |
6. Systems, Subsystems and
Equipment |
| TOWARDS TRAJECTORY
PREDICTION AND OPTIMISATION FOR ENERGY EFFICIENCY OF AN AIRCRAFT WITH
ELECTRICAL AND HYDRAULIC ACTUATION SYSTEMS |
ICAS 2012-6.7.3 |
6. Systems, Subsystems and
Equipment |
| APACHE : INTEGRATED HYBRID
FUEL CELL SYSTEM FOR 2-SEAT ALL ELECTRIC AIRCRAFTS PROPULSION |
ICAS 2012-6.7.4 |
6. Systems, Subsystems and
Equipment |
| INVESTIGATION IN THE DYNAMIC
FORCE EQUALIZATION OF DISSIMILAR REDUNDANT ACTUATION SYSTEMS OPERATING IN
ACTIVE/ACTIVE MODE |
ICAS 2012-6.8.1 |
6. Systems, Subsystems and
Equipment |
| PRELIMINARY STUDY OF EMA
LANDING GEAR ACTUATION |
ICAS 2012-6.8.2 |
6. Systems, Subsystems and
Equipment |
| MODEL BASED DESIGN AND
EXPERIMENTAL VALIDATION OF ELECTRO-MECHANIC ACTUATOR SYSTEMS FOR A NOSE
LANDING GEAR |
ICAS 2012-6.8.3 |
6. Systems, Subsystems and
Equipment |
| FIELD-OF-VIEW, DETECTION
RANGE, AND FALSE ALARM TRADE-OFFS IN VISION-BASED AIRCRAFT DETECTION |
ICAS 2012-6.9.1 |
6. Systems, Subsystems and
Equipment |
| THE SMART SKIES PROJECT:
ENABLING TECHNOLOGIES FOR FUTURE AIRSPACE ENVIRONMENTS |
ICAS 2012-6.9.2 |
6. Systems, Subsystems and
Equipment |
| CONTROL AUGMENTATION SYSTEM
FOR REMOTE STEERING UAV |
ICAS 2012-6.9.3 |
6. Systems, Subsystems and
Equipment |
| PARAMETRIC STUDY OF RAIM
PERFORMANCE USING NEARLY UNIFORMLY DISTRIBUTED REFERENCE POINTS ON THE
EARTH’S SURFACE |
ICAS 2012-6.9.4 |
6. Systems, Subsystems and
Equipment |
| AN OVERVIEW OF THE DEICING
AND ANTIICING TECHNOLOGIES |
ICAS2012-6.5ST: |
6. Systems, Subsystems and
Equipment |
| ELECTROMECHANICAL ACTUATOR
(EMA) ADVANCED TECHNOLOGIES FOR FLIGHT CONTROLS |
ICAS2012-6.8ST: |
6. Systems, Subsystems and
Equipment |
| A PLANAR ANTENNA ARRAY
MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC |
ICAS2012-6.11ST: |
6. Systems, Subsystems and
Equipment |
| ANALYZING AND MODELING OF
JAMMING DESTROY FACTOR |
ICAS2012-P6.1 |
6. Systems, Subsystems and
Equipment |
| A NEW METHOD OF CALCULATION
THE DELAY TIME OF MULTI-CREW MEMBER EJECTION |
ICAS2012-P6.2 |
6. Systems, Subsystems and
Equipment |
| ADVANCED DISPLAY AND
POSITION ANGLES MEASUREMENT SYSTEMS |
ICAS2012-P6.3 |
6. Systems, Subsystems and
Equipment |
| DEVELOPMENT OF A
HYBRID-ELECTRIC POWER-SYSTEM MODEL FOR A SMALL SURVEILLANCE AIRCRAFT |
ICAS2012-P6.4 |
6. Systems, Subsystems and
Equipment |
| HIDDEN MARKOV MODEL
PARAMETER ESTIMATION FOR MULTIPLE DIM TARGET DETECTION |
ICAS2012-P6.5 |
6. Systems, Subsystems and
Equipment |
| A NOVEL ELECTRICAL SERVO
VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
ICAS2012-P6.6 |
6. Systems, Subsystems and
Equipment |
| DISTRIBUTED
OPTICAL FIBRE SMART SENSORS FOR ADVANCE SENSING SYSTEMS IN AEROSPACE VEHICLES |
ICAS2012-P6.7 |
6. Systems, Subsystems and
Equipment |
| DESIGN, ANALYSIS AND
MANUFACTURING OF A THERMOPLASTIC UD CF-PEEK SLAT |
ICAS 2012-6.1.1 |
7. Systems Engineering and
Supply Chain |
| SENSOR AND
REAL-TIME-PROCESS-SIMULATION GUIDED AUTOCLAVE PROCESS CONTROL FOR COMPOSITE
PRODUCTION |
ICAS 2012-6.1.2 |
7. Systems Engineering and
Supply Chain |
| IMPROVING THE PRODUCTION
QUALITY OF THE ADVANCED AUTOMATED FIBER PLACEMENT PROCESS BY MEANS OF ONLINE
PATH CORRECTION |
ICAS 2012-6.1.3 |
7. Systems Engineering and
Supply Chain |
| A SCENARIO-BASED APPROACH TO
DEVELOP REPRESENTATIVE TRAFFIC ENVIRONMENTS FOR OPERATIONAL AIRCRAFT
EVALUATION |
ICAS 2012-6.3.1 |
7. Systems Engineering and
Supply Chain |
| A COMPETITIVE AND
REAL-OPTIONS FRAMEWORK FOR THE ECONOMIC ANALYSIS OF LARGE AEROSPACE PROGRAMS |
ICAS 2012-6.3.2 |
7. Systems Engineering and
Supply Chain |
| THE DESIGN AND ENGINEERING
ENGINE. TOWARDS A MODULAR SYSTEM FOR COLLABORATIVE AIRCRAFT DESIGN |
ICAS 2012-6.3.3 |
7. Systems Engineering and
Supply Chain |
| OPTIMIZING DESIGN
SPECIFICATIONS FROM AIRCRAFT MARKET ECONOMICS |
ICAS 2012-6.3.4 |
7. Systems Engineering and
Supply Chain |
| MULTI-CRITERIA DECISION
ANALYSIS TECHNIQUES IN AIRCRAFT CONCEPTUAL DESIGN PROCESS |
ICAS 2012-6.4.1 |
7. Systems Engineering and
Supply Chain |
| AUTOMATIC FLATTENING OF THREE-DIMENSIONAL WIRING HARNESSES FOR
MANUFACTURING |
ICAS 2012-6.4.2 |
7. Systems Engineering and
Supply Chain |
| A NON-WEIGHT BASED,
MANUFACTURING INFLUENCED DESIGN (MIND) METHODOLOGY FOR PRELIMINARY DESIGN |
ICAS 2012-6.4.3 |
7. Systems Engineering and
Supply Chain |
| A METHODOLOGY FOR PARAMETRIC
PRODUCTION PLANNING IN PRELIMINARY AIRCRAFT DESIGN |
ICAS 2012-6.4.4 |
7. Systems Engineering and
Supply Chain |
| THE DEVELOPMENT OF PRODUCT
AND ASSEMBLY CONCEPTS FOR AIRCRAFT CABIN INTEGRATION |
ICAS 2012-9.9.1 |
7. Systems Engineering and
Supply Chain |
| METHODOLOGY FOR THE DESIGN
OF UNMANNED AIRCRAFT PRODUCT FAMILIES |
ICAS 2012-9.9.2 |
7. Systems Engineering and
Supply Chain |
| DESIGN OF UNMANNED AIR
SYSTEMS FOR USE IN SEARCH AND RESCUE IN THE NORTH ATLANTIC |
ICAS 2012-9.9.3 |
7. Systems Engineering and
Supply Chain |
| MODEL BASED DEFINITION
WITHIN RELOCATION OF AIRCRAFT PRODUCTION |
ICAS 2012-9.9.4 |
7. Systems Engineering and
Supply Chain |
| SCIENCE AND TECHNOLOGY MAP
ANALYSIS OF AEROSPACE ENGINEERING |
ICAS2012-P7.1 |
7. Systems Engineering and
Supply Chain |
| HALA!: TOWARDS HIGHER LEVELS
OF AUTOMATION IN ATM. POSITION PAPER -STATE OF THE ART AND RESEARCH AGENDA |
ICAS 2012-10.1.1 |
8. Air Transport System
Efficiency |
| AUTOMATED CONFLICT-FREE
PLANNING: EXPERIMENTS ON REAL AIR TRAFFIC DATA |
ICAS 2012-10.1.2 |
8. Air Transport System
Efficiency |
| INTEROPERABILITY OF MILITARY
AIRCRAFT VERSUS FUTURE AIR NAVIGATION SYSTEM (FANS) |
ICAS 2012-10.1.3 |
8. Air Transport System
Efficiency |
| AIRPORT CAPACITY
REPRESENTATION BASED ON AIRSIDE SIMULATIONS |
ICAS 2012-10.10.1 |
8. Air Transport System
Efficiency |
| AIRCRAFT FLIGHT TRAJECTORY
DEVIATION IN THE STANDARD INSTRUMENT DEPARTURES. OPERATORS PENALTIES |
ICAS 2012-10.10.2 |
8. Air Transport System
Efficiency |
| NUMERICAL STUDY OF THE
EFFECTS OF CROSS-WIND ON THE JET BLAST DEFORMATION |
ICAS 2012-10.10.3 |
8. Air Transport System
Efficiency |
| PREDICTION OF AIRPORT DELAYS
BASED ON NON-LINEAR CONSIDERATIONS OF AIRPORTS SYSTEMS |
ICAS 2012-10.10.4 |
8. Air Transport System
Efficiency |
| ENHANCING THE "LAST
MILE" COMMUNICATIONS AT AIRPORTS |
ICAS 2012-10.10.5 |
8. Air Transport System
Efficiency |
| A BASIC STUDY ON EFFICIENCY IN JAPANESE
AIRSPACE |
ICAS 2012-10.2.1 |
8. Air Transport System
Efficiency |
| A PRACTICAL, ROUTE-BASED
APPROACH TO AIRSPACE CAPACITY MANAGEMENT |
ICAS 2012-10.2.2 |
8. Air Transport System
Efficiency |
| DELPHI SURVEY 'LEVEL OF
SERVICE FOR AVIATION INFRASTRUCTURE MARKETS?' |
ICAS 2012-10.2.3 |
8. Air Transport System
Efficiency |
| A COMPARISON OF
4D-TRAJECTORY OPERATIONS ENVISIONED FOR 'NEXTGEN' AND 'SESAR', SOME
PRELIMINARY FINDINGS |
ICAS 2012-10.3.1 |
8. Air Transport System
Efficiency |
| IMPROVEMENTS FOR OPTIMUM
PROFILE SCHEDULING OF USER PREFERRED TRAJECTORIES |
ICAS 2012-10.3.2 |
8. Air Transport System
Efficiency |
| AIRCRAFT 4D CONTRACT BASED
OPERATION: THE 4DCO-GC PROJECT |
ICAS 2012-10.3.3 |
8. Air Transport System
Efficiency |
| OPTIMIZATION OF RUNWAY
CAPACITY UTILIZATION IN THE CASE OF GENERAL PARETO CURVE |
ICAS 2012-10.3.4 |
8. Air Transport System
Efficiency |
| DYNAMIC WEATHER ROUTES: A
WEATHER AVOIDANCE SYSTEM FOR NEAR-TERM TRAJECTORY-BASED OPERATIONS |
ICAS 2012-10.4.1 |
8. Air Transport System
Efficiency |
| DYNAMIC SEPARATION MINIMA
COUPLED WITH WAKE VORTEX PREDICTIONS IN DEPENDENT RUNWAY CONFIGURATIONS |
ICAS 2012-10.4.2 |
8. Air Transport System
Efficiency |
| PILOT CONVECTIVE WEATHER
DECISION MAKING IN EN ROUTE AIRSPACE |
ICAS 2012-10.4.3 |
8. Air Transport System
Efficiency |
| OPTIMIZING INBOUND AIRCRAFT
STREAMS USING AIRCRAFT DERIVED DATA AND RTA FUNCTIONALITY |
ICAS 2012-10.4.4 |
8. Air Transport System
Efficiency |
| A PERSONAL PLANE AIR
TRANSPORTATION SYSTEM: THE PPLANE PROJECT |
ICAS 2012-10.5.1 |
8. Air Transport System
Efficiency |
| RESOLVING OFF-NOMINAL
SITUATIONS IN SCHEDULE-BASED TERMINAL AREA OPERATIONS: RESULTS FROM A
HUMAN-IN-THE-LOOP SIMULATION |
ICAS 2012-10.5.2 |
8. Air Transport System
Efficiency |
| CONCEPT OF INTEGRATION FOR
UAS OPERATIONS IN THE NAS |
ICAS 2012-10.7.1 |
8. Air Transport System
Efficiency |
| FUNDAMENTAL CHARACTERISTICS
OF DECENTRALIZED AIR TRAFFIC FLOW CONTROL IN HIGH DENSITY CORRIDOR |
ICAS 2012-10.7.2 |
8. Air Transport System
Efficiency |
| DESIGN OF FLIGHT AVOIDANCE
MANOEUVRE ALPHABETS FOR MIXED CENTRALISED-DECENTRALISED SEPARATION MANAGEMENT |
ICAS 2012-10.7.3 |
8. Air Transport System
Efficiency |
| ESTIMATING TIME TO LOSS OF
SEPARATION WITH UNCERTAIN POSITION AND VELOCITY MEASUREMENTS |
ICAS 2012-10.7.4 |
8. Air Transport System
Efficiency |
| A PROBABILITY ASSESSMENT OF
THE FLIGHT SAFETY RELEVANT TO COLLISION AVOIDANCE |
ICAS 2012-10.7.5 |
8. Air Transport System
Efficiency |
| IMPLEMENTING TIME BASED CDA
OPERATIONS IN A MEDIUM-HIGH DENSITY ATM ENVIRONMENT |
ICAS 2012-10.8.1 |
8. Air Transport System
Efficiency |
| A STUDY ON FINDING A
SUBSTITUTE TO THE FIRST COME- FIRST SERVED RULE APPLIED TO AIRCRAFT
SEQUENCING |
ICAS 2012-10.8.2 |
8. Air Transport System
Efficiency |
| ANALYZING SEPARATION LOSS
EVENTS IN TWO-PAIRED AIRCRAFT TRAILING CONDUCTING AIRBORNE TIME SPACING BASED
CONTINUOUS DESCENT ARRIVAL |
ICAS 2012-10.8.3 |
8. Air Transport System
Efficiency |
| AIRCRAFT TAXIING MODEL AT
CONGESTED AIRPORTS |
ICAS 2012-10.9.1 |
8. Air Transport System
Efficiency |
| DYNAMIC TURNAROUND
MANAGEMENT IN A HIGHLY AUTOMATED AIRPORT ENVIRONMENT |
ICAS 2012-10.9.2 |
8. Air Transport System
Efficiency |
| THE GENERALIZED ARRIVAL
PLANNER (GARP): MODELING AND ANALYSIS FOR ARRIVAL PLANNING |
ICAS 2012-10.9.3 |
8. Air Transport System
Efficiency |
| A MICRO-SIMULATION OF
AIRPORT PASSENGERS WITH ADVANCED TRAITS |
ICAS 2012-10.9.4 |
8. Air Transport System
Efficiency |
| AN ASSET FOR IMPROVED
EFFICIENCY AND PUNCTUALITY IN AIR TRANSPORT |
ICAS 2012-11.7.5 |
8. Air Transport System
Efficiency |
| FLIGHT TRAJECTORY
OPTIMIZATION FOR AN EFFICIENT AIR TRANSPORTATION SYSTEM |
ICAS 2012-5.8.3 |
8. Air Transport System
Efficiency |
| A CASE STUDY OF ARRIVAL AND
DEPARTURE MANAGERS COOPERATION FOR REDUCING AIRBORNE HOLDING TIMES AT
DESTINATION AIRPORTS |
ICAS2012-10.1ST: |
8. Air Transport System
Efficiency |
| DEVELOPMENT
OF THE OPTIMIZED APPROACH AND LANDING TRAJECTORY FOR FUTURE AIR TRANSPORT
SYSTEM |
ICAS2012-P8.1 |
8. Air Transport System
Efficiency |
| EVALUATING FLEXIBILITY IN
AIRPORT CAPACITY-ENHANCING TECHNOLOGY INVESTMENTS |
ICAS2012-P8.2 |
8. Air Transport System
Efficiency |
| CONTINUOUS DESCENT
TRAJECTORY WITH OPTIMUM ARRIVAL TIME CONTROLLABILITY |
ICAS2012-P8.3 |
8. Air Transport System
Efficiency |
| BRISBANE AIRPORT'S NEW
PARALLEL RUNWAY |
ICAS2012-P8.4 |
8. Air Transport System
Efficiency |
| PATH PLANNING FOR MULTI
HELICOPTER COORDINATED RESCUE |
ICAS2012-P8.5 |
8. Air Transport System
Efficiency |
| BALANCING OPERATOR PRIVACY
AND FUTURE AIRSPACE SURVEILLANCE |
ICAS2012-P8.6 |
8. Air Transport System
Efficiency |
| A
META-HEURISTIC APPROACH TO SIMULATE TAXI OPERATIONS |
ICAS2012-P8.7 |
8. Air Transport System
Efficiency |
| DEVELOPMENT OF MOBILE
PASSIVE SECONDARY SURVEILLANCE RADAR |
ICAS2012-P8.8 |
8. Air Transport System
Efficiency |
| AUTOMATION GUIDELINES FOR
INTRODUCING SURVIVABILITY ANALYSIS IN FUTURE FIGHTER AIRCRAFT |
ICAS 2012-9.1.1 |
9. Safety and Security |
| THE EFFECT OF CROSSWIND ON
ENGINE INGESTION DURING TAKEOFFS FROM WATER CONTAMINATED RUNWAYS |
ICAS 2012-9.1.2 |
9. Safety and Security |
| AIRCRAFT EMERGENCY
EVACUATION SIMULATION USING ANT COLONY OPTIMIZATION |
ICAS 2012-9.1.3 |
9. Safety and Security |
| RUNWAY CONFLICT ALERTING
DURING TAKE-OFF AND LANDING: ADVISORY OR DIRECTIVE? |
ICAS 2012-9.10.1 |
9. Safety and Security |
| EFFECTIVE SAFETY MANAGEMENT
SYSTEMS FOR ACCIDENT PREVENTION |
ICAS 2012-9.10.2 |
9. Safety and Security |
| INTERVAL MANAGEMENT WITH
SPACING TO PARALLEL DEPENDENT RUNWAYS (IMSPIDR) EXPERIMENT AND RESULTS |
ICAS 2012-9.10.3 |
9. Safety and Security |
| CORRESPONDENCE AND
CLUSTERING METHODS FOR IMAGE-BASED WING-TIP COLLISION AVOIDANCE TECHNIQUES |
ICAS 2012-9.10.4 |
9. Safety and Security |
| THE NEED FOR A COLLISION
PREVENTION SYSTEM FOR THE PUSHBACK OF AIRCRAFT |
ICAS 2012-9.10.5 |
9. Safety and Security |
| DEVELOPMENT OF AN INTEGRATED
INFORMATION MANAGEMENT SYSTEM FOR AIRCRAFT STRUCTURAL TEST PROGRAMS |
ICAS 2012-9.2.1 |
9. Safety and Security |
| COMPUTATIONAL ASPECTS OF
PROBABILISTIC ASSESSMENT OF UAS ROBUST AUTONOMY |
ICAS 2012-9.2.2 |
9. Safety and Security |
| APPLICATION OF THE RANGE
SAFETY TEMPLATE TOOLKIT TO UAS RISK HAZARD ANALYSES SUPPORTING AIRWORTHINESS
REGULATION |
ICAS 2012-9.2.3 |
9. Safety and Security |
| EVALUATION OF MISSION
PERFORMANCE AND SAFETY FOR FIRE-FIGHTING AMPHIBIAN |
ICAS 2012-9.3.1 |
9. Safety and Security |
| FINAL RESULTS OF THE SUPRA
PROJECT: IMPROVED SIMULATION OF UPSET RECOVERY |
ICAS 2012-9.3.2 |
9. Safety and Security |
| THE GLARE EVALUATION METHOD
FOR CIVIL AIRPLANE FLIGHT DECK |
ICAS 2012-9.3.3 |
9. Safety and Security |
| UNRELIABLE AIRSPEED – MAKING
VALID ASSUMPTIONS ON FLIGHT CREW PERFORMANCE |
ICAS 2012-9.3.4 |
9. Safety and Security |
| DETERMINATION OF AIRBORNE
RECORDED PARAMETERS FOR COMPREHENSIVE FLIGHT DATA MONITORING PROGRAM |
ICAS 2012-9.4.1 |
9. Safety and Security |
| EVALUATION OF ROBUST
AUTONOMY AND IMPLICATIONS ON UAS DESIGN |
ICAS 2012-9.4.2 |
9. Safety and Security |
| INVESTIGATING THE SAFETY
IMPACT OF TIME BUFFERS IN CURRENT TMA ARRIVAL OPERATIONS |
ICAS 2012-9.4.3 |
9. Safety and Security |
| CATEGORIZATION OF UNRELIABLE
AIRSPEED EVENTS USING RASMUSSEN’S HUMAN PERFORMANCE MODEL |
ICAS 2012-9.4.4 |
9. Safety and Security |
| DEVELOPMENT AND EVALUATION
OF FATIGUE AND DROWSINESS PREDICTOR |
ICAS 2012-9.6.1 |
9. Safety and Security |
| EMERGING WIRELESS
TECHNOLOGIES TO IMPROVE AIRBORNE AVIATION SECURITY |
ICAS 2012-9.6.2 |
9. Safety and Security |
| APPLICATION AND POTENTIALS
OF WIRELESS COMMUNICATION TECHNOLOGIES IN PASSENGER AIR TRANSPORT FROM AN
AVIATION SECURITY STANDPOINT |
ICAS 2012-9.6.3 |
9. Safety and Security |
| SHIELDING COSMIC RADIATION
IN AIR TRAFFIC |
ICAS 2012-9.6.4 |
9. Safety and Security |
| INSIDE THE PILOTS MIND:
VISUAL INFORMATION USE IN MANUAL AIRCRAFT LANDINGS |
ICAS 2012-9.7.1 |
9. Safety and Security |
| INNOVATION IN MAN MACHINE
INTERFACES: USE OF 3D CONFORMAL SYMBOLS IN THE DESIGN OF FUTURE HUDS (HEAD UP
DISPLAYS) |
ICAS 2012-9.7.2 |
9. Safety and Security |
| A CAPABILITY FRAMEWORK FOR
MULTIPLE HETEROGENEOUS UAVS: FROM A MISSION COMMANDER'S PERSPECTIVE |
ICAS 2012-9.7.3 |
9. Safety and Security |
| HMIAC – SURVEY ON
HUMAN-MACHINE INTERACTION IN AIRCRAFT COCKPITS |
ICAS 2012-9.7.4 |
9. Safety and Security |
| THE AFFECT OF SCREEN SIZE ON
MISSION COMMANDER’S SITUATION AWARENESS |
ICAS 2012-9.7.5 |
9. Safety and Security |
| LEGAL AND TECHNICAL
IMPLICATIONS OF THE SAFETY RECOMMENDATIONS ISSUED IN THE FINAL REPORTS OF THE
CIVIL AIR ACCIDENTS AND INCIDENTS INVESTIGATIONS |
ICAS2012-9.4ST: |
9. Safety and Security |
| DEVELOPMENT OF LAPTOP PC
TOOL WITH VISUAL PROJECTION FOR FLIGHT MANAGEMENT TRAINING |
ICAS2012-9.10ST: |
9. Safety and Security |
| RELIABILITY ANALYSIS OF
AIRCRAFT SYSTEM ARCHITECTURES |
ICAS2012-P9.1 |
9. Safety and Security |
| RISK ASSESSMENT MODELLING
FOR EVALUATING SAFETY AND IMPACT ON BUSINESS VIA A 3D RISK MATRIX |
ICAS2012-P9.2 |
9. Safety and Security |
| CURFEWS AT INTERNATIONAL
AIRPORTS - A STUDY OF CURRENT PRACTICE |
ICAS 2012-10.5.3 |
10. Challenge of the Environment |
| FLIGHT TESTING OF NOISE
ABATING RNP PROCEDURES AND STEEP APPROACHES |
ICAS 2012-4.9.1 |
10. Challenge of the Environment |
| GBAS CURVED APPROACH
PROCEDURES: ADVANTAGES, CHALLENGES AND APPLICABILITY |
ICAS 2012-4.9.2 |
10. Challenge of the Environment |
| A PROPOSAL FOR REVISED
APPROACHES AND PROCEDURES TO MALTA INTERNATIONAL AIRPORT |
ICAS 2012-4.9.3 |
10. Challenge of the Environment |
| MODELLING AIR TRAFFIC IMPACT
ON LOCAL AIR QUALITY WITH IESTA AND ADMS-AIRPORT: VALIDATION USING FIELD
MEASUREMENTS ON A REGIONAL AIRPORT |
ICAS 2012-4.9.4 |
10. Challenge of the Environment |
| DEVELOPING OPTIMAL AIRLINE
FLEETS UNDER ENVIRONMENTAL AND CAPACITY CONSTRAINTS |
ICAS 2012-7.10.1 |
10. Challenge of the Environment |
| UNCERTAINTY QUANTIFICATION
IN THE DEVELOPMENT OF AVIATION OPERATIONS TO REDUCE AVIATION EMISSIONS AND
CONTRAILS |
ICAS 2012-7.10.2 |
10. Challenge of the Environment |
| AN INTERDISCIPLINARY
APPROACH FOR A VIRTUAL AIR-TRAFFIC SYSTEM SIMULATION FOR SUBJECTIVE
ASSESSMENT IN VR ENVIRONMENTS |
ICAS 2012-7.10.3 |
10. Challenge of the Environment |
| ICAO’S BALANCED APPROACH TO
NOISE MANAGEMENT AND ITS INFLUENCE ON THE ECONOMIC IMPACT OF AIR
TRANSPORTATION |
ICAS 2012-7.10.4 |
10. Challenge of the Environment |
| PREDICTING NOISE EXPOSURE
FOR FLIGHT CREW MEMBERS |
ICAS 2012-7.10.5 |
10. Challenge of the Environment |
| MEASURING SYSTEM-WIDE
IMPACTS OF NEW AIRCRAFT ON THE ENVIRONMENT |
ICAS 2012-7.11.1 |
10. Challenge of the Environment |
| RESEARCH ON ESTIMATING
METHOD OF FUEL AND EMISSIONS USING NEURAL NETWORKS IN LTO CYCLE FOR
PRELIMINARY AIRCRAFT DESIGN |
ICAS 2012-7.11.2 |
10. Challenge of the Environment |
| JAXA’S ENVIRONMENT CONSCIOUS
AIRCRAFT TECHNOLOGY PROGRAM PLAN |
ICAS 2012-7.11.3 |
10. Challenge of the Environment |
| PROGRESS AND PERSPECTIVES OF
ELECTRIC AIR TRANSPORT |
ICAS 2012-8.6.1 |
10. Challenge of the Environment |
| ALTERNATIVE AVIATION FUEL
FEEDSTOCK: THE MICROALGAE SOLUTION? |
ICAS 2012-8.6.2 |
10. Challenge of the Environment |
| IMPACT OF ALTERNATIVE FUELS
ON ENGINE PERFORMANCE AND CO2-EMISSIONS |
ICAS 2012-8.6.3 |
10. Challenge of the Environment |
| PRODUCTION
OF BIO-FUEL FROM ALGAE BIOMASS, NANNOCHLOROPSIS OCULATA, FOR ADDITION TO
KEROSENE JET A-1 |
ICAS 2012-8.6.4 |
10. Challenge of the Environment |
| PROBING THE LIMITS - NEW
OPPORTUNITIES IN THERMOELASTIC STRESS ANALYSIS |
ICAS 2012-12.1.1 |
11. Operations and Sustainment |
| OUTLINE OF AIRCRAFT
STRUCTURE HEALTH AND USAGE MONITORING SYSTEMS AND METHODS USED FOR THEIR
REALIZATIONS |
ICAS 2012-12.1.2 |
11. Operations and Sustainment |
| THE INTEGRATION METHOD OF
FAULT DIAGNOSIS AND HEALTH ASSESSMENT FOR UAV SYSTEM |
ICAS 2012-12.1.3 |
11. Operations and Sustainment |
| EFFECT OF OFF-NORMAL LOADING
ON THE BOND STRENGTH MEASUREMENT OF BONDED REPAIRS |
ICAS 2012-12.2.1 |
11. Operations and Sustainment |
| CRITICAL ASSESSMENT OF
FAILURE CRITERION FOR ADHESIVELY BONDED COMPOSITE JOINT REPAIR DESIGN |
ICAS 2012-12.2.2 |
11. Operations and Sustainment |
| EVALUATION AND CORRELATION
OF INTER-LABORATORY RESULTS FROM A RAIN EROSION TEST CAMPAIGN |
ICAS 2012-12.2.3 |
11. Operations and Sustainment |
| SYSTEM ANALYSIS OF
PROGNOSTICS AND HEALTH MANAGEMENT SYSTEMS FOR FUTURE TRANSPORT AIRCRAFT |
ICAS 2012-12.3.1 |
11. Operations and Sustainment |
| AGEING AIRCRAFT SYSTEMS
& COST EFFECTIVE SAFETY |
ICAS 2012-12.3.2 |
11. Operations and Sustainment |
| A FEASIBILITY STUDY FOR
MULTI-MATERIAL RETROFITTABLE ENERGY ABSORBING STRUCTURE FOR AGED HELICOPTER
SUBFLOOR |
ICAS 2012-12.3.3 |
11. Operations and Sustainment |
| QUANTITATIVE FRACTOGRAPHY
MARKERS FOR DETERMINING FATIGUE CRACK GROWTH RATES IN ALUMINIUM AND TITANIUM
AIRCRAFT STRUCTURES |
ICAS 2012-12.4.1 |
11. Operations and Sustainment |
| FATIGUE DESIGN PROCEDURE OF
LONGITUDINAL AND TRANSVERSE FUSELAGE JOINTS |
ICAS 2012-12.4.2 |
11. Operations and Sustainment |
| FATIGUE LIFE ANALYSIS OF
MAIN LANDING GEAR PULL-ROD OF THE
FIGHTER JET AIRCRAFT |
ICAS 2012-12.4.3 |
11. Operations and Sustainment |
| DEVELOPING THE USE OF
NEURAL-NETWORK TEST TECHNOLOGY FROM AVIONICS TO WIRING SYSTEMS |
ICAS 2012-12.5.1 |
11. Operations and Sustainment |
| INVESTIGATION OF AIRBORNE
PRODUCT EXPENDING DYNAMIC CALIBRATION LIFE METHODS |
ICAS 2012-12.5.2 |
11. Operations and Sustainment |
| INITIAL RESULTS FROM DSTO’S
CORROSION STRUCTURAL INTEGRITY ROADMAP |
ICAS 2012-12.6.1 |
11. Operations and Sustainment |
| INTRODUCTION OF A STRUCTURE
INTEGRITY PROGRAM FOR A MILITARY TRAINER AIRCRAFT |
ICAS 2012-12.6.2 |
11. Operations and Sustainment |
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