| REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS |
ICAS 2008-0.1 |
General Lectures |
| ENVIRONMENTAL IMPACT OF AVIATION: A REVIEW OF SELECTED US RESEARCH EFFORTS |
ICAS 2008-0.2 |
General Lectures |
| AVIATION CLIMATE IMPACT - A SUMMARY OF ONGOING EUROPEAN RESEARCH PROGRAMMES |
ICAS 2008-0.3 |
General Lectures |
| ICAS - THE FIRST 50 YEARS |
ICAS 2008-0.4 |
General Lectures |
| EUROFIGHTER/TYPHOON PROGRAMME |
ICAS 2008-0.5 |
General Lectures |
| INNOVATIONS IN COMBUSTION TECHNOLOGY FOR PROPULSION |
ICAS 2008-0.6 |
General Lectures |
| RECENT DEVELOPMENT OF STRUCTURAL HEALTH MONITORING TECHNOLOGIES FOR AIRCRAFT COMPOSITE STRUCTURES |
ICAS 2008-0.7 |
General Lectures |
| THE BOEING 787 DREAMLINER PROGRAMME |
ICAS 2008-0.8 |
General Lectures |
| MULTIDISCIPLINARY DESIGN, ANALYSIS, AND OPTIMIZATION TOOL DEVELOPMENT USING GENETIC ALGORITHM |
ICAS 2008-1.1.1 |
1. Aircraft and Systems Integration |
| UNCERTAINTIES AT THE CONCEPTUAL STAGE: MULTILEVEL MULTIDISCIPLINARY DESIGN AND OPTIMIZATION APPROACH |
ICAS 2008-1.1.2 |
1. Aircraft and Systems Integration |
| MULTI-DISCIPLINARY DESIGN EXPLORATION FOR WINGLET |
ICAS 2008-1.1.3 |
1. Aircraft and Systems Integration |
| DESIGN OF A SMALL SUPERSONIC TRANSPORT AIRCRAFT WITH HIGH ENVIRONMENTAL CONSTRAINTS |
ICAS 2008-1.10.1 INVITED |
1. Aircraft and Systems Integration |
| SUPERSONIC AIRCRAFT FORMATION FLYING TO INCREASE FLIGHT EFFICIENCY |
ICAS 2008-1.10.2 |
1. Aircraft and Systems Integration |
| CONCEPTUAL DESIGN OF A STOL REGIONAL-JET WITH HYBRID PROPULSION SYSTEM |
ICAS 2008-1.2.1 |
1. Aircraft and Systems Integration |
| DESIGN AND AERODYNAMIC ANALYSIS OF A LIGHT TWIN ENGINE PROPELLER AIRCRAFT |
ICAS 2008-1.2.2 |
1. Aircraft and Systems Integration |
| CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION |
ICAS 2008-1.2.3 |
1. Aircraft and Systems Integration |
| AN APPROACH FOR MULTI-CRITERIA DECISION MAKING METHOD SELECTION AND DEVELOPMENT |
ICAS 2008-1.3.1 |
1. Aircraft and Systems Integration |
| A NEW SYSTEMS ANALYSIS: PERSPECTIVES ON SYSTEM-OF-SYSTEMS AND REGIONAL TRANSPORTATION PROOF-OF-CONCEPT STUDY |
ICAS 2008-1.3.2 |
1. Aircraft and Systems Integration |
| PARAMETRIC SYSTEM EFFECTIVENESS ANALYSIS USING ARTIFICIAL NEURAL NETWORKS FOR BATTLE MANAGEMENT |
ICAS 2008-1.3.3 |
1. Aircraft and Systems Integration |
| LONG TERM AIRCRAFT PROJECT AND TECHNOLOGY EVALUATION UNDER THE UNCERTAINTY OF FUTURE SCENARIOS |
ICAS 2008-1.3.4 |
1. Aircraft and Systems Integration |
| DESIGN OF NEXT GENERATION UNMANNED AIR SYSTEMS - ISSUES AND OPPORTUNITIES |
ICAS 2008-1.4.1 INVITED |
1. Aircraft and Systems Integration |
| DESIGN AND DEVELOPMENT OF THE ECLIPSE AND DEMON DEMONSTRATOR UAVS |
ICAS 2008-1.4.2 |
1. Aircraft and Systems Integration |
| PRELIMINARY DESIGN OF A JOINED WING HALE UAV |
ICAS 2008-1.4.3 |
1. Aircraft and Systems Integration |
| A NEW AIRCRAFT CONCEPT: THE COMBAT MALE |
ICAS 2008-1.4.4 |
1. Aircraft and Systems Integration |
| AUTONOMOUS AERIAL OBSERVATION SYSTEM FOR DISASTER RESPONSE USING ELECTRIC DUCTED FAN MAVS |
ICAS 2008-1.4.5 |
1. Aircraft and Systems Integration |
| FLAPPING-WING TECHNOLOGY: THE POTENTIAL FOR AIR VEHICLE PROPULSION AND AIRBORNE POWER GENERATION |
ICAS 2008-1.5.1 |
1. Aircraft and Systems Integration |
| MINI UAV DESIGN AND OPTIMIZATION FOR LONG ENDURANCE MISSION |
ICAS 2008-1.5.2 |
1. Aircraft and Systems Integration |
| DEVELOPMENT OF FLAPPING WING MICRO AIR VEHICLE |
ICAS 2008-1.5.3 |
1. Aircraft and Systems Integration |
| INNOVATIVE APPROACH FOR FUTURE AIRCRAFT DEVELOPMENT AT IAI |
ICAS 2008-1.6.1 |
1. Aircraft and Systems Integration |
| DEVELOPMENT AND VALIDATION OF A NEXT-GENERATION CONCEPTUAL AERO-STRUCTURAL SIZING SUITE |
ICAS 2008-1.6.2 |
1. Aircraft and Systems Integration |
| CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN |
ICAS 2008-1.6.3 |
1. Aircraft and Systems Integration |
| INCLUSION OF ENGINE RELATED PARAMETERS IN CONCEPTUAL DESIGN OF MORPHING AIRCRAFT |
ICAS 2008-1.6.4 |
1. Aircraft and Systems Integration |
| EVOLUTION OF EMBRAER’S CIVIL AIRCRAFT |
ICAS 2008-1.7.1 INVITED |
1. Aircraft and Systems Integration |
| NACRE EUROPEAN PROJECT PROGRESS SUMMARY |
ICAS 2008-1.7.2 |
1. Aircraft and Systems Integration |
| RE-INVENTING THE LEGEND: THE DEVELOPMENT OF THE 747-8 |
ICAS 2008-1.7.3 |
1. Aircraft and Systems Integration |
| AERODYNAMIC AND AERO-ACOUSTIC DESIGN OF MODERN TILT-ROTORS: THE ONERA EXPERIENCE |
ICAS 2008-1.7.4 |
1. Aircraft and Systems Integration |
| GRIPEN, PROGRAM OVERVIEW AND FUTURE DEVELOPMENT |
ICAS 2008-1.7.5 |
1. Aircraft and Systems Integration |
| AIRCRAFT CONCEPTUAL DESIGN AUTOMATION |
ICAS 2008-1.8.1 |
1. Aircraft and Systems Integration |
| COMPUTATIONAL TOOLS FOR AIRCRAFT SYSTEM ANALYSIS AND OPTIMIZATION |
ICAS 2008-1.8.2 |
1. Aircraft and Systems Integration |
| UNCERTAINTY QUANTIFICATION FOR CAPABILITY-BASED SYSTEMS-OF-SYSTEMS DESIGN |
ICAS 2008-1.8.3 |
1. Aircraft and Systems Integration |
| A SYSTEMATIC APPROACH IN AIRCRAFT CONFIGURATION DESIGN OPTIMIZATION |
ICAS 2008-1.9.1 (AIAA 2008-8926) |
1. Aircraft and Systems Integration |
| DOMAIN SPECIFIC MODELING LANGUAGES TO SUPPORT MODEL-DRIVEN ENGINEERING OF AIRCRAFT SYSTEMS |
ICAS 2008-1.9.2 (AIAA 2008-8927) |
1. Aircraft and Systems Integration |
| FUNCTION BASED ARCHITECTURE DESIGN SPACE DEFINITION AND EXPLORATION |
ICAS 2008-1.9.3 (AIAA 2008-8928) |
1. Aircraft and Systems Integration |
| ADVANCED GENERAL AVIATION DESIGN WITH TRANSPORTATION ARCHITECTURE ANALYSIS |
ICAS 2008-1.9.4 (AIAA 2008-8929) |
1. Aircraft and Systems Integration |
| AERO-STRUCTURAL MDO OF A SPAR-TANK-TYPE WING FOR AIRCRAFT CONCEPTUAL DESIGN |
ICAS2008-1.1 ST: |
1. Aircraft and Systems Integration |
| DEVELOPMENT OF A SMALL UNMANNED AIR VEHICLE WITH MINIMUM SENSORS PHILOSOPHY |
ICAS2008-1.4 ST: |
1. Aircraft and Systems Integration |
| THEORETICAL AND EXPERIMENTAL INVESTIGATION OF ENERGY EXTRACTION FROM ATMOSPHERIC TURBULENCE |
ICAS2008-1.5 ST: |
1. Aircraft and Systems Integration |
| EMAT APPLIED IN THE AVIATION INDUSTRY |
ICAS2008-P1.1 (AIAA 2008-8870) |
1. Aircraft and Systems Integration |
| DEVELOPMENT OF UNMANNED AERIAL VEHICLE IN BPPT |
ICAS2008-P1.10 |
1. Aircraft and Systems Integration |
| MISSION DECISION-MAKING METHOD OF MULTI-AIRCRAFT COOPERATIVELY ATTACKING MULTI-TARGET BASED ON SITUATIONAL ASSESSMENT |
ICAS2008-P1.2 |
1. Aircraft and Systems Integration |
| AIRCRAFT PARAMETRIC 3D MODELING AND PANEL CODE ANALYSIS FOR CONCEPTUAL DESIGN |
ICAS2008-P1.3 |
1. Aircraft and Systems Integration |
| A MULTIDISCIPLINARY OPTIMIZATION METHOD APPLIED TO AIRCRAFT DESIGN |
ICAS2008-P1.4 |
1. Aircraft and Systems Integration |
| AN UPDATING PROGRAM FOR UNDERGRADUATE AIRCRAFT CONCEPTUAL AND PRELIMINARY DESIGN COURSE |
ICAS2008-P1.5 |
1. Aircraft and Systems Integration |
| AIRPLANE DESIGN: A MUST IN AERONAUTICAL ENGINEERING EDUCATION |
ICAS2008-P1.6 |
1. Aircraft and Systems Integration |
| POTENTIALS OF LIGHTER-THAN-AIR TECHNOLOGY IN FUTURE MARKETS – AN EVALUATION |
ICAS2008-P1.7 |
1. Aircraft and Systems Integration |
| PROMISING FUTURE AIRCRAFT CONCEPT – ESTOL |
ICAS2008-P1.8 |
1. Aircraft and Systems Integration |
| DEVELOPMENT OF A COAXIAL ROTOR MAV FOR INDOOR APPLICATION |
ICAS2008-P1.9 |
1. Aircraft and Systems Integration |
| A HYBRID, DYNAMIC LARGE EDDY SIMULATION METHOD |
ICAS 2008-2.1.1 |
2. Aerodynamics |
| HIGH-ORDER LARGE EDDY SIMULATION AROUND 2-D AEROFOIL WITH HIGH-LIFT DEVICE |
ICAS 2008-2.1.2 |
2. Aerodynamics |
| COMPUTATIONAL INVESTIGATION AND DESIGN OF COMPLIANT MEMBRANE WINGS FOR BIOLOGICALLY INSPIRED FLIGHT VEHICLES |
ICAS 2008-2.10.1 |
2. Aerodynamics |
| A COMPARISON OF NUMERICAL RANS SIMULATIONS AND FLOW FIELD MEASUREMENTS OF AN OSCILLATING AIRFOIL FOR FLAPPING WING PROPULSION |
ICAS 2008-2.10.2 |
2. Aerodynamics |
| SMALL DISTURBANCE NAVIER-STOKES COMPUTATIONS FOR LOW ASPECT RATIO WING PITCHING OSCILLATIONS |
ICAS 2008-2.10.3 |
2. Aerodynamics |
| PREDICTION OF HELICOPTER MANEUVER LOADS USING A TIGHTLY COUPLED CFD/CSD ANALYSIS |
ICAS 2008-2.10.4 |
2. Aerodynamics |
| NUMERICAL SIMULATION OF 3D FLAPPING WING BASED ON CHIMERA METHOD |
ICAS 2008-2.10.5 |
2. Aerodynamics |
| EFFICIENT APPROACH FOR MULTIPOINT AERODYNAMIC WING DESIGN OF BUSINESS JET AIRCRAFT |
ICAS 2008-2.11.1 |
2. Aerodynamics |
| OPTIMISING HIGH-EFFICIENCY RUDDERS FOR TRANSPORT AIRCRAFT FUEL BURN REDUCTION |
ICAS 2008-2.11.2 |
2. Aerodynamics |
| AERODYNAMIC OPTIMIZATION OF AIRCRAFT CONFIGURATIONS WITH MULTIDISZIPLINARY ASPECTS |
ICAS 2008-2.11.3 |
2. Aerodynamics |
| COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA |
ICAS 2008-2.2.1 |
2. Aerodynamics |
| NUMERICAL SIMULATION OF ICE ACCRETION ON MULTIPLE-ELEMENT AIRFOIL SECTIONS |
ICAS 2008-2.2.2 |
2. Aerodynamics |
| NUMERICAL AERODYNAMIC OPTIMISATIONS OF 3D HIGH-LIFT CONFIGURATIONS |
ICAS 2008-2.2.3 |
2. Aerodynamics |
| APPLICATION OF A NAVIER-STOKES CODE TO THE SIMULATIONS OF HIGH-LIFT DEVICES USING UNSTRUCTURED GRIDS |
ICAS 2008-2.2.4 |
2. Aerodynamics |
| INTERFACE CONDITIONS OF FINITE-DIFFERENCE COMPACT SCHEMES FOR COMPUTATIONAL AEROACOUSTICS |
ICAS 2008-2.3.1 |
2. Aerodynamics |
| EULER INVERSE THROUGHFLOW MODEL BASED ON AN IMPLICIT UPWIND TIME MARCHING TECHNIQUE |
ICAS 2008-2.3.2 |
2. Aerodynamics |
| THE APPLICATION OF ASEXUAL DNA ALGORITHM TO AIRFOIL DESIGN |
ICAS 2008-2.3.3 |
2. Aerodynamics |
| AN AERODYNAMIC OPTIMIZATION FRAMEWORK BASED ON GENETIC ALGORITHMS |
ICAS 2008-2.3.4 |
2. Aerodynamics |
| LOW-BOOM AND LOW-DRAG OPTIMIZATION FOR THE TWIN-ENGINE SILENT SUPERSONIC TECHNOLOGY DEMONSTRATOR |
ICAS 2008-2.4.1 |
2. Aerodynamics |
| FLIGHT TEST RESULTS AT TRANSONIC REGION ON SUPERSONIC EXPERIMENTAL AIRPLANE (NEXST-1) |
ICAS 2008-2.4.2 |
2. Aerodynamics |
| WING DESIGN OF SUPERSONIC TRANSPORT BY A MULTI-POINT OPTIMIZATION METHOD |
ICAS 2008-2.4.3 |
2. Aerodynamics |
| AERODYNAMIC DESIGN OF THREE-DIMENSIONAL BIPLANE WINGS FOR LOW-WAVE DRAG SUPERSONIC FLIGHT |
ICAS 2008-2.4.4 |
2. Aerodynamics |
| COMPARISON OF SHOCK WAVE INTERACTION FOR THE THREE-DIMENSIONAL SUPERSONIC BIPLANE WITH DIFFERENT PLANAR SHAPES |
ICAS 2008-2.4.5 |
2. Aerodynamics |
| A CFD STUDY OF UCAV 1303 BASELINE MODEL AT CRUISE MACH NUMBERS |
ICAS 2008-2.5.1 |
2. Aerodynamics |
| EXPERIENCES OF GRID GENERATION AND STEADY/UNSTEADY VISCOUS COMPUTATIONS FOR COMPLEX GEOMETRIES |
ICAS 2008-2.5.2 |
2. Aerodynamics |
| A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS |
ICAS 2008-2.5.3 |
2. Aerodynamics |
| A LAYER PAVEMENT MODEL TO SIMULATE ROUGHNESS FEATURES IN ICE ACCRETION NUMERICAL SIMULATION |
ICAS 2008-2.6.1 |
2. Aerodynamics |
| IHAAA STORE SEPARATION FROM CAVITY (SSC) PROJECT |
ICAS 2008-2.6.2 |
2. Aerodynamics |
| NUMERICAL SIMULATION OF VISCOUS FLOWS AROUND LIFTING BODIES OF COMPLICATED CONFIGURATION |
ICAS 2008-2.6.3 |
2. Aerodynamics |
| PREDICTION OF SUPERCOOLED DROPLET IMPINGEMENT ON HELICOPTER ROTOR BLADES |
ICAS 2008-2.6.4 |
2. Aerodynamics |
| CONTROL OF A SWEPT WING TAILLESS AIRCRAFT THROUGH WING MORPHING |
ICAS 2008-2.7.1 |
2. Aerodynamics |
| AERODYNAMIC DESIGN OF THE A400M HIGH-LIFT SYSTEM |
ICAS 2008-2.7.2 INVITED |
2. Aerodynamics |
| SINGLE VERSUS MULTIPLE WINGLETS: NUMERICAL AND EXPERIMENTAL INVESTIGATION |
ICAS 2008-2.7.3 |
2. Aerodynamics |
| COMPUTATIONS FOR LAMINAR FLOW CONTROL IN SWEPT-WING BOUNDARY LAYERS |
ICAS 2008-2.7.4 |
2. Aerodynamics |
| FLIGHT EXPERIMENTS ON SWEPT WING TRANSITION USING DISTRIBUTED ROUGHNESS |
ICAS 2008-2.7.5 |
2. Aerodynamics |
| TOWARDS AERODYNAMIC OPTIMISATION OF AN AEROELASTIC WING USING DOMAIN ELEMENT PARAMETERISATION |
ICAS 2008-2.8.1 |
2. Aerodynamics |
| APPLICATION OF AN HYBRID OPTIMIZATION APPROACH IN THE DESIGN OF LONG ENDURANCE AIRFOILS |
ICAS 2008-2.8.2 |
2. Aerodynamics |
| ON AIRCRAFT PERFORMANCE IMPROVEMENT BY USING WINGLETS |
ICAS 2008-2.8.3 |
2. Aerodynamics |
| TRANSONIC STORE SEPARATION STUDIES ON THE SAAB GRIPEN AIRCRAFT USING COMPUTATIONAL AERODYNAMICS |
ICAS 2008-2.9.1 |
2. Aerodynamics |
| TARGETING PODS EFFECTS ON STORE SEPARATION CHARACTERISTICS: A JOINT NRC-IAR/USNAVY CFD EFFORT |
ICAS 2008-2.9.2 |
2. Aerodynamics |
| STORE SEPARATION TRAJECTORY SIMULATION FOR THE HIGH SPEED ANTI-RADIATION DEMONSTRATOR (HSAD) FROM THE F-4 AIRCRAFT |
ICAS 2008-2.9.3 |
2. Aerodynamics |
| TARGETING POD EFFECTS ON WEAPONS RELEASE FROM THE F-18C HORNET |
ICAS 2008-2.9.4 |
2. Aerodynamics |
| ESTIMATION OF SUPERSONIC STAGE SEPARATION AERODYNAMICS OF WINGED-BODY LAUNCH VEHICLES USING RESPONSE SURFACE METHODS |
ICAS 2008-3.1.1 |
2. Aerodynamics |
| PROPELLER SLIPSTREAM INVESTIGATION USING THE FOKKER F27 WIND TUNNEL MODEL WITH FLAPS DEFLECTED |
ICAS 2008-3.1.2 |
2. Aerodynamics |
| THE APPLICATION OF SEMI-EMPIRICAL STORE RELEASE SIMULATION FOR THE OPTIMIZATION OF GRID SURVEY WIND TUNNEL TESTING |
ICAS 2008-3.1.3 |
2. Aerodynamics |
| SUPPRESSING BOUNDARY LAYER SEPARATION BY UNSTEADY EXCITATION OF MINI-SCALE LEADING-EDGE FLAPS |
ICAS 2008-3.10.1 |
2. Aerodynamics |
| ACTIVE CANCELLATION OF TOLLMIEN-SCHLICHTING INSTABILITIES UP TO M = 0.40 |
ICAS 2008-3.10.2 |
2. Aerodynamics |
| TRANSVERSAL INJECTED SYNTHETIC JETS FOR WALL TURBULENCE CONTROL |
ICAS 2008-3.10.3 |
2. Aerodynamics |
| SEPARATION CONTROL BY SYNTHETIC JET ACTUATOR IN STRAIGHT BLADE CASCADE |
ICAS 2008-3.10.4 |
2. Aerodynamics |
| VORTEX SHEDDING FROM A ROTATING CIRCULAR CYLINDER AT MODERATE SUB-CRITICAL REYNOLDS NUMBERS AND HIGH VELOCITY RATIO |
ICAS 2008-3.10.5 |
2. Aerodynamics |
| FLOW CONTROL TECHNIQUES FOR TRANSPORT AIRCRAFT |
ICAS 2008-3.11.1 |
2. Aerodynamics |
| ACTIVE SEPARATION CONTROL ON A SLATLESS 2D HIGH-LIFT WING SECTION |
ICAS 2008-3.11.2 |
2. Aerodynamics |
| AERODYNAMIC STALL SUPPRESSION ON AEROFOIL SECTIONS USING PASSIVE AIR JET VORTEX GENERATORS |
ICAS 2008-3.11.3 |
2. Aerodynamics |
| DEVELOPMENT & APPLICATION OF MODERN MEASUREMENT TECHNIQUES FOR PRESSURIZED CRYOGENIC WIND TUNNELS |
ICAS 2008-3.2.1 |
2. Aerodynamics |
| INVESTIGATION OF THE FLOW IN A RECTANGULAR CAVITY USING TOMOGRAPHIC AND TIME-RESOLVED PIV |
ICAS 2008-3.2.2 |
2. Aerodynamics |
| AEROACOUSTIC NOISE MEASUREMENTS IN AERODYNAMIC LOW-SPEED WIND TUNNELS |
ICAS 2008-3.2.3 |
2. Aerodynamics |
| NUMERICAL STUDY OF A PITOT PROBE WITH FIVE-HOLE PYRAMIDAL HEAD FOR SUPERSONIC FLIGHT TEST |
ICAS 2008-3.2.4 |
2. Aerodynamics |
| THE SECOND INTERNATIONAL VORTEX FLOW EXPERIMENT (VFE-2): RESULTS OF THE FIRST PHASE 2003 - 2008 |
ICAS 2008-3.3.1 INVITED |
2. Aerodynamics |
| VORTEX BEHAVIORS OF CRANKED ARROW WING CONFIGURATIONS WITH DIFFERENT WING PLANFORMS |
ICAS 2008-3.3.2 |
2. Aerodynamics |
| INVESTIGATION OF THE FLOW OVER NACELLE/PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION |
ICAS 2008-3.3.3 |
2. Aerodynamics |
| FOREBODY VORTEX CONTROL ON HIGH PERFORMANCE AIRCRAFT USING PWM-CONTROLLED PLASMA ACTUATORS |
ICAS 2008-3.3.4 |
2. Aerodynamics |
| FIN BUFFET CHARACTERISTICS OF ADVANCED TRAINER AIRCRAFT |
ICAS 2008-3.4.1 |
2. Aerodynamics |
| 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 |
2. Aerodynamics |
| MEASUREMENT OF UNSTEADY AERODYNAMIC FORCES OF 3D FLAPPING WING IN HOVERING TO FORWARD FLIGHT |
ICAS 2008-3.4.3 |
2. Aerodynamics |
| A SMALL SCALE PITCH-PLUNGE FLUTTER MODEL FOR ACTIVE FLUTTER CONTROL RESEARCH |
ICAS 2008-3.4.4 |
2. Aerodynamics |
| APPLICATION OF SEMICONDUCTOR STRAIN GAUGES IN MEASUREMENTS OF DYNAMIC STABILITY DERIVATIVES IN THE T-38 WIND TUNNEL |
ICAS 2008-3.4.5 |
2. Aerodynamics |
| AERODYNAMIC INVESTIGATIONS ON A GENERIC FAN-IN-WING CONFIGURATION |
ICAS 2008-3.5.1 |
2. Aerodynamics |
| COMPUTATIONAL FLUID DYNAMICS AND EXPERIMENTAL INVESTIGATION OF AIRPLANE STALL DYNAMICS WITH WING CONTAMINATION |
ICAS 2008-3.5.2 |
2. Aerodynamics |
| NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THE AERODYNAMICS OF UNCONVENTIONAL W-LEADING EDGE REVERSED DELTA WING IN GROUND EFFECT |
ICAS 2008-3.5.3 |
2. Aerodynamics |
| NUMERICAL ANALYSIS OF THIN-WALLED STRUCTURES IN HYPERSONIC FLOW REGIME |
ICAS 2008-3.6.1 |
2. Aerodynamics |
| ANALYSIS OF THERMOCHEMICAL MODELING AND SURFACE CATALYTICITY IN SPACE VEHICLES REENTRY |
ICAS 2008-3.6.2 |
2. Aerodynamics |
| NUMERICAL STUDY OF THE EFFECT OF THE OPPOSING JET ON REDUCTION OF AERODYNAMIC HEATING WITH DIFFERENT NOSE CONFIGURATIONS |
ICAS 2008-3.6.3 |
2. Aerodynamics |
| HEAT TRANSFER ON HYPERSONIC BLUNT BODIES WITH GAS INJECTION |
ICAS 2008-3.6.4 |
2. Aerodynamics |
| A WALL SHEAR STRESS MEASUREMENT TECHNIQUE USING THE THERMAL WAKES OF SMALL HEATED SPOTS |
ICAS 2008-3.7.1 |
2. Aerodynamics |
| PERFORMANCE DEGRADATION OF A SIMULATED ICE CONTAMINATED AIRFOIL BY SUPER-COOLED DROPLETS |
ICAS 2008-3.7.2 |
2. Aerodynamics |
| IN-FLIGHT EXPERIMENTS FOR DELAYING LAMINAR-TURBULENT TRANSITION ON A LAMINAR WING GLOVE |
ICAS 2008-3.7.3 |
2. Aerodynamics |
| PIV FLOW MEASUREMENTS FOR A HIGH LIFT AIRFOIL WITH LEADING EDGE ICE |
ICAS 2008-3.7.4 |
2. Aerodynamics |
| EXPERIMENTAL STUDY ON INTERFERENCE FLOW OF A SUPERSONIC BUSEMANN BIPLANE USING PRESSURE-SENSITIVE PAINT TECHNIQUE |
ICAS 2008-3.7.5 |
2. Aerodynamics |
| THE EFFECTS OF WALL ROUGHNESS ON THE TURBULENT BOUNDARY LAYER |
ICAS 2008-3.8.1 |
2. Aerodynamics |
| WHITE LIGHT SKIN-FRICTION AND GAS DENSITY MEASUREMENTS AROUND A SUPERSONIC FOREBODY |
ICAS 2008-3.8.2 |
2. Aerodynamics |
| LAMINAR-TURBULENT TRANSITION CORRELATION IN SUPERSONIC/ HYPERSONIC FLOW – ATTACHED VERSUS SEPARATED FLOW |
ICAS 2008-3.8.3 |
2. Aerodynamics |
| VORTEX WAKE INVESTIGATION BEHIND A WING-FLAP MODEL WITH JET SIMULATION |
ICAS 2008-3.9.1 |
2. Aerodynamics |
| VORTEX BLOB METHOD AS VISUALIZATION TOOL FOR MULTI-ELEMENT AIRFOIL FLOWS OPTIMIZATION |
ICAS 2008-3.9.2 |
2. Aerodynamics |
| UNSTEADY PROPULSIVE CHARACTERISTICS OF BIOFOILS MOVING IN A VERY LOW-REYNOLDS NUMBER FLOW |
ICAS 2008-3.9.3 |
2. Aerodynamics |
| ON THE EFFECTS ON NOISE OF GROUND REFLECTION AND ATMOSPHERIC ATTENUATION ON THE NOISE OF HELICOPTERS |
ICAS 2008-3.9.4 |
2. Aerodynamics |
| INVESTIGATION OF SEPARATION CONTROL FOR LOW-PRESSURE TURBINES USING CFD |
ICAS 2008-4.4.2 |
2. Aerodynamics |
| KRYLOV RECYCLING TECHNIQUES FOR UNSTEADY SIMULATION OF TURBULENT AERODYNAMIC FLOWS |
ICAS2008-2.1 ST: |
2. Aerodynamics |
| LARGE EDDY SIMULATION AROUND 2-D AIRFOIL WITH NATURAL TRANSITION AT HIGH REYNOLDS NUMBERS |
ICAS2008-2.1 ST: |
2. Aerodynamics |
| UNSTEADY AERODYNAMIC ANALYSIS OF HELICOPTER ROTOR BY USING THE TIME-DOMAIN PANEL METHOD |
ICAS2008-2.10 ST: |
2. Aerodynamics |
| COMPRESSIBLE FLUID-FLOW ALE FORMULATION ON CHANGING TOPOLOGY MESHES FOR AEROELASTIC SIMULATIONS |
ICAS2008-2.10 ST: |
2. Aerodynamics |
| AERODYNAMIC OPTIMIZATION OF A BLENDED WING BODY |
ICAS2008-2.11 ST: |
2. Aerodynamics |
| OVERVIEW OF THE NUMERICAL SIMULATIONS OF THE HIGH-LIFT-DEVICE NOISE MEASUREMENT MODEL |
ICAS2008-2.2 ST: |
2. Aerodynamics |
| HYBRIDIZATION OF HETEROGENEOUS 3D CFD DISCRETIZATIONS VIA DIRECT FLUX OPTIMIZATION |
ICAS2008-2.3 ST: |
2. Aerodynamics |
| MODERN MATHEMATICAL METHODS IN AERONAUTICAL SCIENCES |
ICAS2008-2.3 ST: |
2. Aerodynamics |
| WING CONFIGURATION EFFECTS ON FLOW FIELD AND AERODYNAMIC PER-FORMANCE OF SUPERSONIC BIPLANE FOR SONIC-BOOM REDUCTION |
ICAS2008-2.4 ST: |
2. Aerodynamics |
| AERODYNAMICS CHARACTERISTICS OF HYPERSONIC VEHICLE IN NEAR SPACE |
ICAS2008-2.5 ST: |
2. Aerodynamics |
| CFD RESEARCH FOR AIR-TO-AIR MISSILE WITH LATERAL JET CONTROL |
ICAS2008-2.64 ST: |
2. Aerodynamics |
| PASSIVE, ACTIVE AND ADAPTIVE SYSTEMS FOR WING VORTEX DRAG REDUCTION |
ICAS2008-2.7 ST: |
2. Aerodynamics |
| LOW REYNOLDS NUMBER TANDEM OR DIAMOND WING UAV AERODYNAMICS CENTER RESEARCH BASED ON RESPONSE SURFACE METHOD |
ICAS2008-3.1 ST: |
2. Aerodynamics |
| INVESTIGATION ON THE EFFECT OF HYDRODYNAMIC MEMS ON AIRFOIL |
ICAS2008-3.10 ST: |
2. Aerodynamics |
| DELTA-WING VORTEX CONTROL BY APEX STRAKE AND MICRO LEADING-EDGE FLAP |
ICAS2008-3.3 ST: |
2. Aerodynamics |
| EXPERIMENTAL RESEARCH OF FLAPPING-WING PROPULSION FOR MICRO AIR VEHICLES |
ICAS2008-3.4 ST: |
2. Aerodynamics |
| NUMERICAL SIMULATION OF FLAPPING WING AERODYNAMIC PERFORMANCE UNDER GUST WIND CONDITIONS |
ICAS2008-3.5 ST: |
2. Aerodynamics |
| AN EXPERIMENTAL AND COMPUTATIONAL COMPARISON OF THE LOW SPEED AERODYNAMICS OF SQUARE AND CIRCULAR SECTIONED BODIES |
ICAS2008-3.5 ST: |
2. Aerodynamics |
| THE INVESTIGATION OF DEPENDENCE OF LOW FREQUENCY MOTION ON UPSTREAM FLOW CONDITIONS IN HYPERSONIC FLOWS |
ICAS2008-3.7 ST: |
2. Aerodynamics |
| ESTIMATION OF THE INFLUENCE OF PROFILE ERROR ON AERODYNAMIC PERFORMANCE FOR LOW-REYNOLDS-NUMBER AIRFOILS |
ICAS2008-3.7 ST: |
2. Aerodynamics |
| EXCRESCENCES EFFECTS IN AERODYNAMICS |
ICAS2008-3.8 ST: |
2. Aerodynamics |
| AN APPROXIMATION METHOD FOR THE NUMERICAL SIMULATION ON UNSTEADY FLOWS AROUND SMALL-DISPLACEMENT MOVING OBJECTS |
ICAS2008-3.9 ST: |
2. Aerodynamics |
| AN EXPERIMENTAL AND COMPUTATIONAL STUDY OF LOW RE NUMBER TRANSITIONAL FLOWS OVER AN AEROFOIL WITH LEADING EDGE SLAT |
ICAS2008-P2.1 (AIAA 2008-8877) |
2. Aerodynamics |
| RESEARCH ON MONITORING AND CONTROL SYSTEM BASED PLC IN THE NF-6 WIND TUNNEL |
ICAS2008-P2.10 |
2. Aerodynamics |
| WIND TUNNEL AND COMPUTIONAL INVESTIGATION OF SIMULATED CONTAMINATION ON AIRFOIL |
ICAS2008-P2.11 |
2. Aerodynamics |
| ON RESULTS’ ACCURACY AT TWO-DIMENSIONAL WIND TUNNEL TESTING |
ICAS2008-P2.12 |
2. Aerodynamics |
| DRAG AND FLOW REGIMES ASSOCIATED WITH RECTANGULAR CAVITIES AT YAW AT LOW SPEEDS |
ICAS2008-P2.13 |
2. Aerodynamics |
| RELATION BETWEEN TRAILING EDGE NOISE AND BOUNDARY LAYER INSTABILITY |
ICAS2008-P2.14 |
2. Aerodynamics |
| THE QUEST FOR A TRULY PARSIMONIOUS AIRFOIL PARAMETERIZATION SCHEME |
ICAS2008-P2.2 (AIAA 2008-8879) |
2. Aerodynamics |
| NUMERICAL AND EXPERIMENTAL STUDIES OF SHOCK INTERFERENCE IN HYPERSONIC FLOWS NEAR A CYLINDER |
ICAS2008-P2.3 |
2. Aerodynamics |
| A FAST GRID DEFORMATION ALGORITHM AND IT’S APPLICATION |
ICAS2008-P2.4 |
2. Aerodynamics |
| LIFT PREDICTION OF MULTI-ELEMENT AIRFOIL USING DES AND RANS |
ICAS2008-P2.5 |
2. Aerodynamics |
| MODULATION TRANSFER FUNCTION OF STEREO PARTICLE IMAGE VELOCIMETRY TECHNIQUE |
ICAS2008-P2.6 |
2. Aerodynamics |
| SOLUTIONS OF INVISCID AND VISCOUS FLOWS USING STRUCTURED HIGH RESOLUTION ALGORITHMS IN THREE-DIMENSIONS |
ICAS2008-P2.7 |
2. Aerodynamics |
| LARGE-SCALE MANIPULATION OF A TURBULENT BOUNDARY LAYER BY MEANS OF A 2D SYNTHETIC JET |
ICAS2008-P2.8 |
2. Aerodynamics |
| PROTOTYPE OF A STIFF WIND TUNNEL BALANCE WITH SEMICONDUCTOR STRAIN GAUGES AND THERMOCOMPENSATION DONE BY SOFTWARE |
ICAS2008-P2.9 |
2. Aerodynamics |
| A STUDY OF SHEAR LAYER SUB-STRUCTURES IN LEADING EDGE VORTICES USING LASER DOPPLER VELOCIMETRY |
ICAS 2008-2.1.3 |
3. Materials and Structures |
| PROBABILISTIC MODELING OF STRUCTURAL / AEROELASTIC LIFE CYCLE FOR RELIABILITY EVALUATION OF DAMAGE TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.1.1 |
3. Materials and Structures |
| RESEARCH ON FAILURE CRITERION FOR COMPOSITE MATERIALS IN OPTIMIZATION |
ICAS 2008-7.1.2 |
3. Materials and Structures |
| A MULTI-SCALE “MORPHOLOGICAL APPROACH” FOR MODELING THE NON LINEAR BEHAVIOR OF PROPELLANT-LIKE MATERIALS |
ICAS 2008-7.1.3 |
3. Materials and Structures |
| ACTIVE AND PASSIVE STRUCTURAL MEASURES FOR AEROELASTIC WINGLET DESIGN |
ICAS 2008-7.10.1 |
3. Materials and Structures |
| DEVELOPMENT OF A RUDDERLESS AEROELASTIC FIN TECHNOLOGY |
ICAS 2008-7.10.2 |
3. Materials and Structures |
| OPTIMUM AEROELASTIC DESIGN OF A RESONANCE TYPE FLAPPING WING FOR MICRO AIR VEHICLES |
ICAS 2008-7.10.3 |
3. Materials and Structures |
| NUMERICAL SIMULATION OF AN OSCILLATING AND FLEXIBLE AIRFOIL FOR FLAPPING WING PROPULSION WITH FLUID-STRUCTURE INTERACTION |
ICAS 2008-7.10.4 |
3. Materials and Structures |
| TRANSONIC FLUTTER ANALYSIS OF AN AIRFOIL WITH APPROXIMATE BOUNDARY METHOD |
ICAS 2008-7.10.5 |
3. Materials and Structures |
| METHODOLOGY FOR THERMALLY INDUCED LOADING IN STRUCTURAL ANALYSIS ON THE F-35 LIGHTNING II |
ICAS 2008-7.11.1 |
3. Materials and Structures |
| MECHANICS OF COMPOSITES IN LIGHTWEIGHT STRUCTURES: EFFICIENT TESTING AND COMPUTATION ACCOUNTING FOR COMPLEX 3D BEHAVIOUR |
ICAS 2008-7.11.2 |
3. Materials and Structures |
| COLLAPSE BEHAVIOR OF THIN-WALLED CFRP STRUCTURES DUE TO MATERIAL AND GEOMETRIC NONLINEARITIES–EXPERIMENTS AND SIMULATION |
ICAS 2008-7.11.3 |
3. Materials and Structures |
| INVESTIGATION OF ADHESIVELY BONDED COMPOSITE STRUCTURE JOINTS |
ICAS 2008-7.2.1 |
3. Materials and Structures |
| LOADED CARBON COMPOSITE SCARF JOINTS SUBJECT TO QUASI STEADY LATERAL LOADS |
ICAS 2008-7.2.2 |
3. Materials and Structures |
| THERMAL DESIGN UNDER UNCERTAINTIES OF AIRCRAFT STRUCTURES |
ICAS 2008-7.2.3 |
3. Materials and Structures |
| MICROMECHANICAL FEM MODELING OF THERMAL STRESSES IN FUNCTIONALLY GRADED MATERIALS |
ICAS 2008-7.2.4 |
3. Materials and Structures |
| APPROXIMATIONS FOR FULLY ISOTROPIC LAMINATE CONFIGURATIONS |
ICAS 2008-7.3.1 |
3. Materials and Structures |
| THE DESIGN OF POSTBUCKLING COMPOSITE AEROSPACE STRUCTURES ACCOUNTING FOR DAMAGE INITIATION AND GROWTH |
ICAS 2008-7.3.2 |
3. Materials and Structures |
| METAMODELS FOR THE OPTIMIZATION OF DAMAGE-TOLERANT COMPOSITE STRUCTURES |
ICAS 2008-7.3.3 |
3. Materials and Structures |
| CARBON/DYNEEMA INTRALAMINAR HYBRIDS: NEW STRATEGY TO INCREASE IMPACT RESISTANCE OR DECREASE MASS OF CARBON FIBER COMPOSITES |
ICAS 2008-7.3.4 |
3. Materials and Structures |
| STATIC AND FATIGUE ANALYSIS OF AN UPPER WING SKIN WITH EXFOLIATION CORROSION |
ICAS 2008-7.4.1 |
3. Materials and Structures |
| FATIGUE ANALYSIS: THE SUPER-NEUBER TECHNIQUE FOR CORRECTION OF LINEAR ELASTIC FE RESULTS |
ICAS 2008-7.4.2 |
3. Materials and Structures |
| FATIGUE DESIGN OF METALLIC COMPONENTS CONTAINING SURFACE OR INTERNAL DEFECTS |
ICAS 2008-7.4.3 |
3. Materials and Structures |
| FATIGUE BEHAVIOR AND LIFE PREDICTION OF WELDED TITANIUM ALLOY JOINTS |
ICAS 2008-7.4.4 |
3. Materials and Structures |
| EFFECTS OF SUSPENSION WEIGHT ON FIGHTER FATIGUE DAMAGE |
ICAS 2008-7.4.5 |
3. Materials and Structures |
| COHESIVE DISINTEGRATION IN IMPACTED RE-ENTRY SPACE TRANSPORTATION HYBRID STRUCTURES |
ICAS 2008-7.5.1 |
3. Materials and Structures |
| COMPRESSION STRENGTH OF NOTCHED AND IMPACT DAMAGED COMPOSITE LAMINATES |
ICAS 2008-7.5.2 |
3. Materials and Structures |
| PREDICTION OF DELAMINATION IN ADVANCED AEROSPACE COMPOSITE STRUCTURES USING MICRO/MACRO MECHANICS CONSTITUTIVE METHODS |
ICAS 2008-7.5.3 |
3. Materials and Structures |
| FATIGUE CRACK GROWTH PREDICTION OF FIBRE REINFORCED METAL LAMINATES UNDER VARIABLE AMPLITUDE LOADING |
ICAS 2008-7.6.1 |
3. Materials and Structures |
| THE INFLUENCE OF FATIGUE CRACK INITIATION BEHAVIOUR OF FRICTION STIR WELDED JOINTS ON THE DESIGN CRITERIA |
ICAS 2008-7.6.2 |
3. Materials and Structures |
| ESTIMATION OF CRACK TURN PHENOMENON |
ICAS 2008-7.6.3 |
3. Materials and Structures |
| EFFICIENT AEROELASTIC SIMULATION IN A PARAMETRIC PROCEDURE FOR FATIGUE ANALYSIS |
ICAS 2008-7.7.1 |
3. Materials and Structures |
| MONITORING OF OSCILLATORY FAILURE CASES FOR THE REDUCTION OF STRUCTURAL LOADS IN AN AEROELASTIC AIRCRAFT |
ICAS 2008-7.7.2 |
3. Materials and Structures |
| UNIFIED BE-FE AERODYNAMIC-ACOUSTIC-STRUCTURE COUPLING SCHEME FOR ACOUSTIC EFFECTS ON AEROELASTIC STRUCTURES |
ICAS 2008-7.7.3 |
3. Materials and Structures |
| UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING |
ICAS 2008-7.7.4 |
3. Materials and Structures |
| SCALED DOWN MODELS FOR FREE VIBRATION ANALYSIS OF ORTHOGONALLY STIFFENED CYLINDRICAL SHELLS USING SIMILITUDE THEORY |
ICAS 2008-7.7.5 |
3. Materials and Structures |
| DESIGN AND MANUFACTURING OF COMPOSITE CHIRAL STRUCTURES WITH MORPHING CAPABILITIES |
ICAS 2008-7.8.1 |
3. Materials and Structures |
| POST-BUCKLED PRECOMPRESSED ELEMENTS: A NEW CLASS OF FLIGHT CONTROL ACTUATORS ENHANCING MORPHING WING UAVS |
ICAS 2008-7.8.2 |
3. Materials and Structures |
| APPLICATION OF SHAPE OPTIMISATION TO AIRCRAFT WING STRUCTURES |
ICAS 2008-7.8.3 |
3. Materials and Structures |
| FLIGHT VEHICLE COMPOSITE STRUCTURES |
ICAS 2008-7.9.1 (AIAA 2008-8976 ) |
3. Materials and Structures |
| SURVEY OF FEASIBLE NUMERICAL APPROACHES TO ANALYSE THE BEHAVIOUR OF A COMPOSITE SKIN PANEL DURING A WATER IMPACT |
ICAS 2008-7.9.2 |
3. Materials and Structures |
| BWB MILITARY CARGO TRANSPORT FUSELAGE DESIGN AND ANALYSIS |
ICAS 2008-7.9.3 |
3. Materials and Structures |
| THERMAL ASPECTS FOR COMPOSITE STRUCTURES - FROM MANUFACTURING TO IN-SERVICE PREDICTIONS |
ICAS 2008-7.9.4 |
3. Materials and Structures |
| IMPACT CHARACTERISTICS ESTIMATION OF SHORT SUPPORT COLUMNS UNDER CABIN FLOOR |
ICAS 2008-9.4.1 |
3. Materials and Structures |
| A NEGATIVE SELECTION APPROACH TO DETECT DAMAGE IN AERONAUTICAL STRUCTURES WITH CHANGING OPERATING CONDITIONS |
ICAS 2008-9.4.2 |
3. Materials and Structures |
| FE STUDY OF WINDSHIELD SUBJECTED TO HIGH SPEED BIRD IMPACT |
ICAS 2008-9.4.3 |
3. Materials and Structures |
| BIRDSTRIKE ONTO STRUCTURES IN ROTATIONAL MOTION |
ICAS 2008-9.4.4 |
3. Materials and Structures |
| STRUCTURAL MODEL TUNING CAPABILITY IN AN OBJECT-ORIENTED MULTIDISCIPLINARY DESIGN, ANALYSIS, AND OPTIMIZATION TOOL |
ICAS 2008-9.5.1 |
3. Materials and Structures |
| OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING - EXPERIMENTAL VERIFICATION |
ICAS 2008-9.5.2 |
3. Materials and Structures |
| OPTIMIZATION DESIGN ON PLATE-RIB STRUCTURE FOR CERTAIN KINDS OF AIRCRAFT |
ICAS 2008-9.5.3 |
3. Materials and Structures |
| ACTIVE AEROELASTICITY CONCEPT: NOVEL VIEW, METHODOLOGY AND RESULTS |
ICAS 2008-9.6.1 INVITED |
3. Materials and Structures |
| TRANSONIC FLUTTER WIND TUNNEL TESTS OF CONVENTIONAL TWIN-ENGINE TRANSPORT SEMISPAN MODEL |
ICAS 2008-9.6.2 |
3. Materials and Structures |
| DEVELOPMENT AND VALIDATION OF AN INVESTIGATION TOOL FOR NONLINEAR AEROELASTIC ANALYSIS |
ICAS 2008-9.6.3 |
3. Materials and Structures |
| DYNAMIC ANALYSIS OF AEROELASTIC RESPONSE FOR TRANSONIC FLOW WITH NONLINEAR STRUCTURAL MODEL |
ICAS 2008-9.6.4 |
3. Materials and Structures |
| SIMPLIFYING MSD MODELING BY USING CONTINUING DAMAGE ASSUMPTION AND PARAMETRIC STUDY: THE ROLE OF RIVET SQUEEZE FORCE |
ICAS 2008-9.8.1 |
3. Materials and Structures |
| STUDY ON THE RELATIONSHIP BETWEEN CORROSION DAMAGE AND RESIDUAL STRENGTH OF AL 7075-T6 ALLOY |
ICAS 2008-9.8.2 |
3. Materials and Structures |
| AN ANALYTICAL MODEL FOR PREDICTION OF THE STEADY STATE CREEP DEFORMATIONS AND STRESSES OF SHORT FIBER COMPOSITES |
ICAS 2008-9.8.3 |
3. Materials and Structures |
| INFLUENCES INVESTIGATION OF NUMERICAL PARAMETERS AND MESHING ON THE AEROELASTIC RESPONSE |
ICAS2008- P3.4 |
3. Materials and Structures |
| SIZE OPTIMIZATION OF AIRCRAFT STRUCTURES |
ICAS2008-7.11 ST: |
3. Materials and Structures |
| FROM BEAM MODELS TO GLOBAL 3D MODELS FOR ROBUST LANDING GEAR DESIGN |
ICAS2008-7.11 ST: |
3. Materials and Structures |
| INNOVATIVE COMPOSITE STRUCTURES FOR SMALL AIRCRAFT |
ICAS2008-7.3 ST: |
3. Materials and Structures |
| AN ORIGINAL SYSTEM TO MEASURE ADAPTIVE STRUCTURE PARAMETERS USING FIBER OPTIC |
ICAS2008-7.4 ST: |
3. Materials and Structures |
| ON THE DEVELOPMENT OF METHODS AND TECHNIQUES FOR AIRCRAFT STRUCTURAL HEALTH MONITORING |
ICAS2008-7.4 ST: |
3. Materials and Structures |
| IMPACT RESISTANCE, DAMAGE TOLERANCE AND NON-DESTRUCTIVE DAMAGE DETECTION FOR SANDWICH STRUCTURES: ANALYSIS AND TESTING |
ICAS2008-7.5 ST: |
3. Materials and Structures |
| SUITABILITY OF DIFFERENT CRACK GROWTH MODELS FOR ANALYSING MULTI-SITE DAMAGE IN AIRCRAFT STRUCTURAL CONFIGURATIONS |
ICAS2008-7.6 ST: |
3. Materials and Structures |
| PRACTICAL AEROELASTIC CALCULATIONS FOR LIGHT AIRPLANES |
ICAS2008-7.7 ST: |
3. Materials and Structures |
| HEALTH MONITORING FOR AEROCRAFT STRUCTURE SYSTEM BY HARMONIC WAVELET TRANSFORM |
ICAS2008-7.7 ST: |
3. Materials and Structures |
| INTEGRATED PREDICTION OF MACROSCOPIC PROPERTIES OF COMPOSITES BASED ON FINITE ELEMENT COMPUTATIONAL MICROMECHANICS |
ICAS2008-7.9 ST: |
3. Materials and Structures |
| FEM MICRO-MECHANICAL ANALYSIS OF DELAMINATION PHENOMENON IN IMC LAMINATED COMPOSITES USING DAMAGE THEORY |
ICAS2008-9.4 ST: |
3. Materials and Structures |
| AERODYNAMIC SHAPE OPTIMIZATION OF TRANSONIC AEROELASTIC WING BASED ON CONTROL THEORY |
ICAS2008-9.6 ST: |
3. Materials and Structures |
| METHODS FOR CALCULATING THE DAMAGE-RATE OF AIRCRAFT COMPONENT |
ICAS2008-9.8 ST: |
3. Materials and Structures |
| A STUDY ON FATIGUE SCATTER FACTOR OF INDIVIDUAL AIRCRAFT STRUCTURE |
ICAS2008-P3.1 |
3. Materials and Structures |
| ANALYTICAL FORMULATION FOR NON-UNIFORM BEAM FINITE ELEMENT |
ICAS2008-P3.10 |
3. Materials and Structures |
| EXPLOITATION OF OPTIMIZATION SOLUTION FOR DETERMINATION OF WHIRL FLUTTER STABILITY BOUNDARIES |
ICAS2008-P3.2 |
3. Materials and Structures |
| NUMERICAL DEVELOPMENT OF A FLUTTER ACTIVE CONTROL SYSTEM BASED ON PRESSURE FEEDBACK. |
ICAS2008-P3.3 |
3. Materials and Structures |
| THE APPLICATION OF THE MORLET WAVELET ON RESPONSE FILTERING OF THE HELICOPTER CANNON’S RECOIL |
ICAS2008-P3.5 |
3. Materials and Structures |
| ANALYSIS OF THE SCATTERING CHARACTERISTICS FROM DISCONTINUITY SURFACES ON AIRCRAFT USING A MODIFIED MLFMA |
ICAS2008-P3.6 |
3. Materials and Structures |
| IMPACT AND COMPRESSION-AFTER-IMPACT PERFORMANCE OF STITCHED/UNSTITCHED COMPOSITE SANDWICH PANELS WITH A FOAM CORE |
ICAS2008-P3.7 |
3. Materials and Structures |
| MULTIDISCIPLINARY DESIGN OPTIMIZATION OF A SATELLITE BOOM STRUCTURE TO REDUCE WEIGHT AND VIBRATION TRANSMISSION USING GA |
ICAS2008-P3.8 |
3. Materials and Structures |
| EFFECTS OF HIERARCHY ORDER ON NATURAL FREQUENCY AND VIBRATION TRANSMISSION OF SELF-SIMILAR TRUSSES |
ICAS2008-P3.9 |
3. Materials and Structures |
| PERFORMANCE ANALYSIS OF A 3D SCRAMJET INTAKE |
ICAS 2008-4.1.1 |
4. Propulsion |
| 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 |
4. Propulsion |
| TURBULENCE MODELING S AND APPLICATIONS TO AEROSPIKE PLUG NOZZLE |
ICAS 2008-4.1.3 |
4. Propulsion |
| "ACTIVE CORE" - A KEY TECHNOLOGY FOR MORE ENVIRONMENTALLY FRIENDLY AERO ENGINES BEING INVESTIGATED UNDER THE NEWAC PROGRAM |
ICAS 2008-4.2.1 |
4. Propulsion |
| TOWARD ACARE 2020: INNOVATIVE ENGINE ARCHITECTURES TO ACHIEVE THE ENVIRONMENTAL GOALS? |
ICAS 2008-4.2.2 |
4. Propulsion |
| STUDIES ON MDO OF ENGINE DESIGN PARAMETERS WITH MISSION, NOISE & EMISSION CRITERIA AT SSBJ ENGINE CONCEPTUAL DESIGN |
ICAS 2008-4.2.3 |
4. Propulsion |
| NEW METHOD TO ENHANCE THE WEARABILITY OF TITANIUM ALLOY ROTOR BLADE FOR AERO-ENGINE |
ICAS 2008-4.2.4 |
4. Propulsion |
| DEVELOPMENT OF AN INDUSTRIAL SCALE COMBUSTION TEST AND RESEARCH FACILITY FOR ALTERNATIVE FUELS AND FUEL FLEXIBILITY DEMONSTRATION |
ICAS 2008-4.3.1 |
4. Propulsion |
| DEVELOPMENT OF FULL ANNULAR COMBUSTOR FOR SMALL AIRCRAFT JET ENGINE IN JAXA TECHCLEAN PROJECT |
ICAS 2008-4.3.2 |
4. Propulsion |
| NUMERICAL STUDY OF ENERGY UTILIZATION IN NOZZLE/PLUME FLOW-FIELDS OF HIGH-SPEED AIR-BREATHING VEHICLES |
ICAS 2008-4.3.3 |
4. Propulsion |
| FEASIBILITY STUDY ON MULTI-PHASE FLOW SIMULATION OF FUEL INJECTION USING LATTICE BOLTZMANN METHOD |
ICAS 2008-4.3.4 |
4. Propulsion |
| BIRD-STRIKE DAMAGE ANALYSIS IN CONCEPT ADVANCED COMPOSITE FAN BLADES |
ICAS 2008-4.4.1 |
4. Propulsion |
| NUMERICAL INVESTIGATION OF INLET DISTORTION INDUCED SWIRL IN MULTISTAGE FANS |
ICAS 2008-4.4.3 |
4. Propulsion |
| NUMERICAL RESEARCHES ON THE AEROELASTIC PROBLEM OF TURBOMACHINERY |
ICAS 2008-4.4.4 |
4. Propulsion |
| A FLIGHT THRUST DECK FOR THE F100 TURBOFAN OF THE F16 AIRCRAFT |
ICAS 2008-4.5.1 |
4. Propulsion |
| ON-CONDITION MAINTENANCE FOR NON-MODULAR JET ENGINES: AN EXPERIENCE |
ICAS 2008-4.5.2 |
4. Propulsion |
| AERODYNAMIC DESIGN AND ITS VALIDATION OF AN OPEN-TYPE ENGINE RUN-UP FACILITY |
ICAS 2008-4.5.3 |
4. Propulsion |
| PREPARING LP TURBINE TECHNOLOGY FOR MODERN AIRCRAFT ENGINES |
ICAS 2008-4.6.1 |
4. Propulsion |
| EVALUATION OF THE FLOW IN AN INTERMEDIATE TURBINE DUCT AT OFF-DESIGN CONDITIONS |
ICAS 2008-4.6.2 |
4. Propulsion |
| EXPERIMENTAL ANALYSIS OF THE FLOW FIELD IN A ROTATING 'U' CHANNEL |
ICAS 2008-4.6.3 |
4. Propulsion |
| DEVELOPING THE NEXT GENERATION OF GLOBAL GAS TURBINE ENGINEERS |
ICAS 2008-8.10.1 INVITED |
4. Propulsion |
| CUTTING EDGE TECHNOLOGIES FOR DESIGN, PRODUCTION AND REPAIR OF NEXT GENERATION AERO ENGINES |
ICAS 2008-8.10.2 INVITED |
4. Propulsion |
| COUPLED HIGH-FIDELITY ENGINE SYSTEM SIMULATION |
ICAS 2008-8.10.3 INVITED |
4. Propulsion |
| VIRTUAL ENTERPRISE COLLABORATION - BREAKTHROUGH TECHNOLOGIES PROVIDED BY VIVACE |
ICAS 2008-8.10.4 INVITED |
4. Propulsion |
| PROPULSION TECHNOLOGIES FOR THE FUTURE OF AVIATION |
ICAS 2008-8.10.5 INVITED |
4. Propulsion |
| EXPERIMENTAL INVESTIGATION OF SPRAY CHARACTERISTICS OF DOUBLE-BASE SWIRL INJECTOR |
ICAS2008-4.1 ST: |
4. Propulsion |
| A NEW APPROACH FOR CO2 REDUCTION APPLYING STATE-OF-THE-ART ENGINE AND AIRFRAME TECHNOLOGY |
ICAS2008-4.2 ST (AIAA 2008-8974) |
4. Propulsion |
| LASER PROPELLED HYPERSONIC AIR-VEHICLE |
ICAS2008-4.3 ST: |
4. Propulsion |
| UNSTEADY CFD MODELING OF WHOLE GAS TURBINE ENGINE FLOW PASSAGE WITH APPLICATIONS |
ICAS2008-4.4 ST: |
4. Propulsion |
| A RAPID SCENARIO GENERATION TOOL FOR REPEATABLE SIMULATED TRAFFIC CONFLICTS IN FLIGHT SIMULATION |
ICAS 2008-5.1.1 INVITED |
5. Flight Dynamics and Control |
| CESSNA CITATION CJ1 FLIGHT TEST DATA GATHERING AND LEVEL-C SIMULATOR MODEL DEVELOPMENT |
ICAS 2008-5.1.2 |
5. Flight Dynamics and Control |
| MODELING OF THE VISUAL APPROACH TO LANDING USING NEURAL NETWORKS AND FUZZY SUPERVISORY CONTROL |
ICAS 2008-5.1.3 |
5. Flight Dynamics and Control |
| RESEARCH AND DEVELOPMENT FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM – PART 1. INTELLIGENT FLIGHT CONTROL SYSTEM |
ICAS 2008-5.10.1 |
5. Flight Dynamics and Control |
| RESEARCH AND DEVELOPMENT FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM - PART 2 FLIGHT EXPERIMENTS |
ICAS 2008-5.10.2 |
5. Flight Dynamics and Control |
| PERFORMANCE EVALUATION AND HILS TEST OF CONTROL ALLOCATION METHODS FOR RECONFIGURATION CONTROL |
ICAS 2008-5.10.3 |
5. Flight Dynamics and Control |
| NONLINEAR MODEL FOLLOWING RECONFIGURABLE FLIGHT CONTROL SYSTEM |
ICAS 2008-5.10.4 |
5. Flight Dynamics and Control |
| THE INFLUENCE OF FREE - PLAY AND FRICTION IN CONTROL SYSTEM ON AIRCRAFT DYNAMICS |
ICAS 2008-5.10.5 |
5. Flight Dynamics and Control |
| DYNAMIC SIMULATION OF A TOWED DECOY SYSTEM |
ICAS 2008-5.11.1 |
5. Flight Dynamics and Control |
| MODELLING OF STATIC AERODYNAMICS OF HELICOPTER UNDERSLUNG LOADS |
ICAS 2008-5.11.2 |
5. Flight Dynamics and Control |
| GROUND EFFECT MODELING FOR ROTARY-WING SIMULATION |
ICAS 2008-5.11.3 |
5. Flight Dynamics and Control |
| AUTOMATIC FLIGHT CONTROL USING SAMPLED-DATA MIXED H_2/H_INFINITY OPTIMISATION |
ICAS 2008-5.2.1 |
5. Flight Dynamics and Control |
| ALLEVIATION OF ATMOSPHERIC FLOW DISTURBANCE EFFECTS ON AIRCRAFT RESPONSE |
ICAS 2008-5.2.2 |
5. Flight Dynamics and Control |
| MECHANICALLY UNCOUPLED SERVO TABS FOR PRIMARY FLIGHT CONTROLS |
ICAS 2008-5.2.3 |
5. Flight Dynamics and Control |
| RESEARCH ON CONTROL ALLOCATION FOR AIRCRAFTS WITH MULTIPLE CONTROL EFFECTORS |
ICAS 2008-5.2.4 |
5. Flight Dynamics and Control |
| AEROSPACE TRAJECTORY OPTIMIZATION: NOVEL VIEW ON A ROLE OF ATMOSPHERIC FLIGHT |
ICAS 2008-5.3.1 |
5. Flight Dynamics and Control |
| UNIQUE PERFORMANCE CHARACTERISTICS OF SOLAR AIRCRAFT |
ICAS 2008-5.3.2 |
5. Flight Dynamics and Control |
| ON THE MINIMIZATION OF CRUISE DRAG DUE TO PITCH TRIM FOR A FLYING-WING CONFIGURATION |
ICAS 2008-5.3.3 |
5. Flight Dynamics and Control |
| OPTIMIZATION FOR FLIGHT CONTROL SYSTEM WITH CONSTRAINTS SUPPLEMENTED HANDLING QUALITIES |
ICAS 2008-5.3.4 |
5. Flight Dynamics and Control |
| THEORETICAL APPROACH TO DIRECTIONAL CONTROL SENSITIVITY SELECTION |
ICAS 2008-5.4.1 INVITED |
5. Flight Dynamics and Control |
| FEASIBILITY ANALYSIS OF ACHIEVING A STABILIZED APPROACH |
ICAS 2008-5.4.2 |
5. Flight Dynamics and Control |
| CONTROLLABILITY OF BLENDED WING BODY AIRCRAFT |
ICAS 2008-5.4.3 |
5. Flight Dynamics and Control |
| NEURAL NETWORK ANALYSIS OF PILOT MANEUVER DURING LANDING PHASE |
ICAS 2008-5.4.4 |
5. Flight Dynamics and Control |
| RESEARCH ON FUZZY LOGIC PIO DETECTOR |
ICAS 2008-5.4.5 |
5. Flight Dynamics and Control |
| FLIGHT SIMULATORS – ON DIFFERENT PERCEPTIONS OF MANUFACTURERS, AVIATION AUTHORITIES, RESEARCH AND USERS |
ICAS 2008-5.5.1 INVITED |
5. Flight Dynamics and Control |
| RAVEN – A SUBSCALE RADIO CONTROLLED BUSINESS JET DEMONSTRATOR |
ICAS 2008-5.5.2 |
5. Flight Dynamics and Control |
| EXTENDING FMC TEST FOR FLIGHT SIMULATION AND FLIGHT EXPERIMENTS |
ICAS 2008-5.5.3 |
5. Flight Dynamics and Control |
| 3D OBSTACLE AVOIDANCE STRATEGIES FOR UAS (UNINHABITED AERIAL SYSTEMS) MISSION PLANNING AND RE-PLANNING |
ICAS 2008-5.6.1 (AIAA 2008-8962) |
5. Flight Dynamics and Control |
| ROUTE PLANNING FOR RELAY UAV |
ICAS 2008-5.6.2 |
5. Flight Dynamics and Control |
| TRAJECTORY OPTIMISATION FOR AUTONOMOUS VEHICLES: A MINIUAV APPLICATION |
ICAS 2008-5.6.3 |
5. Flight Dynamics and Control |
| ANALYSIS OF DEEPSTALL LANDING FOR UAV |
ICAS 2008-5.6.4 |
5. Flight Dynamics and Control |
| IMPROVEMENT FOR LANDING ON SMALL-MEDIUM AIRPORTS USING FUTURE, AIRCRAFT-AUTONOMOUS GUIDANCE AIDS |
ICAS 2008-5.7.1 INVITED |
5. Flight Dynamics and Control |
| TRAJECTORY CONTROL IMPROVEMENT BASED ON A NONLINEAR DYNAMIC INVERSION APPROACH |
ICAS 2008-5.7.2 |
5. Flight Dynamics and Control |
| INTEGRATED INTERCEPT MISSILE GUIDANCE AND CONTROL WITH TERMINAL ANGLE CONSTRAINT |
ICAS 2008-5.7.3 |
5. Flight Dynamics and Control |
| NONLINEAR FORMATION GUIDANCE LAW WITH ROBUST DISTURBANCE OBSERVER |
ICAS 2008-5.7.4 |
5. Flight Dynamics and Control |
| TRAJECTORY DESIGN OF SILENT SUPERSONIC TECHNOLOGY DEMONSTRATOR (S3TD) |
ICAS 2008-5.7.5 |
5. Flight Dynamics and Control |
| PARAMETER IDENTIFICATION OF FLYING WING WITH SIGNIFICANT DEFORMATION |
ICAS 2008-5.8.1 |
5. Flight Dynamics and Control |
| SIMULATION OF A NON-AXISYMMETRIC UNDERSEA VEHICLE USING A RECURSIVE NEURAL NETWORK |
ICAS 2008-5.8.2 |
5. Flight Dynamics and Control |
| FLIGHT DYNAMICS OF THE FLYING WING |
ICAS 2008-5.8.3 |
5. Flight Dynamics and Control |
| MODELING AND SIMULATION OF FLAPPING WINGS MICRO-AERIAL VEHICLES FLIGHT DYNAMICS |
ICAS 2008-5.9.1 INVITED |
5. Flight Dynamics and Control |
| ROBUST OPTIMAL DESIGN OF AN AUTOPILOT FOR TRANSITIONAL FLIGHTS OF A TAIL-SITTER MINI UAV |
ICAS 2008-5.9.2 |
5. Flight Dynamics and Control |
| GENETIC FUZZY CONTROL FOR AUTONOMOUS DUCTED-FAN VTOL UAV |
ICAS 2008-5.9.3 |
5. Flight Dynamics and Control |
| FLY-BY-WIRE CONTROL OF A HELICOPTER: MULTIBODY MAIN ROTOR MODEL |
ICAS2008-5.11 ST: |
5. Flight Dynamics and Control |
| APPLICATION OF A MODEL UPDATING METHOD TO AN AIRCRAFT LONGITUDINAL STABILITY AUGMENTATION SYSTEM |
ICAS2008-5.2 ST: |
5. Flight Dynamics and Control |
| A PROCEDURE TO DESIGN AIRCRAFT FLIGHT CONTROL LAWS TAKING INTO ACCOUNT ROBUSTNESS USING THE VARIABLE STRUCTURE CONTROL |
ICAS2008-5.4 ST: |
5. Flight Dynamics and Control |
| PARAMETRIC STUDY AND MITIGATION OF PORPOISING IN WATERBORN AIRCRAFTS |
ICAS2008-5.8 ST: |
5. Flight Dynamics and Control |
| DEVELOPMENT OF FLIGHT CONTROL SYSTEM USING EMBEDDED COMPUTER PC-104 |
ICAS2008-P5.1 |
5. Flight Dynamics and Control |
| THE APPLICATION OF AIRBORNE VIDEO TECHNOLOGIES DURING AERIAL REFUELING TEST |
ICAS2008-P5.2 |
5. Flight Dynamics and Control |
| TRAJECTORY TRACKING FOR A NON - CONVENTIONAL UAV |
ICAS2008-P5.3 |
5. Flight Dynamics and Control |
| FLIGHT MECHANICS SIMULATOR FOR ROTORCRAFT DEVELOPMENT |
ICAS2008-P5.4 |
5. Flight Dynamics and Control |
| MODELLING OF THE 3-DOF NONLINEAR AIRCRAFT BEHAVIOUR VIA SMALL STANDARD FORMS |
ICAS2008-P5.5 |
5. Flight Dynamics and Control |
| TERRAIN FOLLOWING FLIGHT REAL-TIME HIL SIMULATION PLATFORM RESEARCH |
ICAS2008-P5.6 |
5. Flight Dynamics and Control |
| TEST FLYING UNMANNED WISE AS A MEANS FOR PROOF OF CONCEPT |
ICAS2008-P5.7 |
5. Flight Dynamics and Control |
| RELIABILITY STUDY OF POWER MODULE BY STOCHASTIC UNCERTAINTY METHOD FOR AN AERONAUTICAL APPLICATION |
ICAS 2008-6.1.1 |
6. Systems, Subsystems and Equipments |
| HEALTH MONITORING FOR COMMERCIAL AIRCRAFT SYSTEMS |
ICAS 2008-6.1.2 |
6. Systems, Subsystems and Equipments |
| HIGH EFFICIENCY, HIGH RELIABILITY 2 KW INVERTER FOR AERONAUTICAL APPLICATION |
ICAS 2008-6.1.3 |
6. Systems, Subsystems and Equipments |
| A QUANTIFIED RELATIONSHIP MATRIX AIDED BY PROBABILISTIC DESIGN AND OPTIMIZATION |
ICAS 2008-6.2.1 |
6. Systems, Subsystems and Equipments |
| METHODOLOGY FOR AIRCRAFT SYSTEM ARCHITECTURE SIZING |
ICAS 2008-6.2.2 |
6. Systems, Subsystems and Equipments |
| AN ADAPTABLE METHODOLOGY FOR AUTOMATION APPLICATION DEVELOPMENT |
ICAS 2008-6.2.3 |
6. Systems, Subsystems and Equipments |
| A SIMULATION FRAMEWORK FOR AIRCRAFT POWER SYSTEMS ARCHITECTING |
ICAS 2008-6.2.4 |
6. Systems, Subsystems and Equipments |
| INVESTIGATION OF LONG-HAUL FLIGHT ATTRIBUTES INFLUENCING PASSENGER'S BOOKING DECISION USING SP DATA |
ICAS 2008-6.3.1 |
6. Systems, Subsystems and Equipments |
| IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY |
ICAS 2008-6.3.2 |
6. Systems, Subsystems and Equipments |
| SCALING OF MIXED CONVECTION IN AIRCRAFT CABINS |
ICAS 2008-6.3.3 |
6. Systems, Subsystems and Equipments |
| EVOLUTION OF FUTURE EQUIPMENTS AND SUB-SYSTEMS FOR THE FUTURE GREEN AIRCRAFT |
ICAS 2008-6.4.1 INVITED |
6. Systems, Subsystems and Equipments |
| MULTIVARIABLE CONTROLLER DESIGN FOR A TRIMMABLE HORIZONTAL STABILIZER ACTUATOR WITH TWO PRIMARY LOAD PATHS |
ICAS 2008-6.4.2 |
6. Systems, Subsystems and Equipments |
| MODELING OF ACOUSTICALLY TREATED NACELLE LIP TRANSPIRATION FLOW ANTI-ICING SYSTEM |
ICAS 2008-6.4.3 |
6. Systems, Subsystems and Equipments |
| SATELLITE-BASED NAVIGATION ARCHITECTURE STUDY FOR AIRCRAFT CATEGORY III LANDINGS |
ICAS 2008-6.4.4 |
6. Systems, Subsystems and Equipments |
| A STUDY OF AN USER AND ENVIRONMENTAL FRIENDLY STORED ENERGY BASED EPU/APU-SYSTEM FOR MILITARY AEROSPACE APPLICATIONS |
ICAS 2008-6.4.5 |
6. Systems, Subsystems and Equipments |
| A VISION OF MORE ELECTRICAL AIRCRAFT AND CURRENT DEVELOPMENTS |
ICAS 2008-6.5.1 INVITED |
6. Systems, Subsystems and Equipments |
| A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS |
ICAS 2008-6.5.2 |
6. Systems, Subsystems and Equipments |
| LATEST DEVELOPMENTS IN ELECTRIAL LANDING SYSTEMS |
ICAS 2008-6.5.3 |
6. Systems, Subsystems and Equipments |
| AUTOMATED GENERATION, SELECTION AND EVALUATION OF ARCHITECTURES FOR ELECTROMECHANICAL ACTUATORS |
ICAS 2008-6.6.1 |
6. Systems, Subsystems and Equipments |
| THERMAL MANAGEMENT OF ELECTROMECHANICAL ACTUATION ON AN ALL-ELECTRIC AIRCRAFT |
ICAS 2008-6.6.2 |
6. Systems, Subsystems and Equipments |
| EVAPORATING COOLANT FOR ON-BOARD COOLING SYSTEMS WITH DIRECT CONDENSATION THROUGH AMBIENT AIR |
ICAS 2008-6.6.3 |
6. Systems, Subsystems and Equipments |
| A DUAL-DUPLEX ELECTROHYDRAULIC SYSTEM FOR THE FLY-BY-WIRE CONTROL OF A HELICOPTER MAIN ROTOR |
ICAS 2008-6.6.4 |
6. Systems, Subsystems and Equipments |
| DESIGN OF A NOVEL INTELLIGENT DATA MANAGEMENT TOOL FOR HEALTH AND USAGE MONITORING SYSTEMS – DESIGN REQUIREMENTS |
ICAS2008-6.1 ST: |
6. Systems, Subsystems and Equipments |
| HOSTED SIMULATION FOR HETEROGENEOUS AIRCRAFT SYSTEM DEVELOPMENT |
ICAS2008-6.2 ST: |
6. Systems, Subsystems and Equipments |
| A NEW EFFICIENT INTERACTIVE MULTI-OBJECTIVE EVOLUTIONARY OPTIMIZATION ALGORITHM AND APPLICATION IN ENGINEERING |
ICAS2008-6.2 ST: |
6. Systems, Subsystems and Equipments |
| THE STATE-OF-THE-ART AND THE FUTURE OF WATER MANAGEMENT WITHIN FUEL TANKS |
ICAS2008-6.4 ST: |
6. Systems, Subsystems and Equipments |
| MULTI-PURPOSE RFID ACCESS CONTROL USING ASYMMETRIC KEY BASED TAG-READER MUTUAL AUTHENTICATION |
ICAS2008-6.4 ST: |
6. Systems, Subsystems and Equipments |
| DEVELOPMENT OF THE DISPLAY DEVICE OF POWER DISTIBUTION SYSTEM (DEVELOPMENT OF THE DEPTH FUSED 3-D DISPLAY FOR AIRCRAFT) |
ICAS2008-6.5 ST: |
6. Systems, Subsystems and Equipments |
| PARAMETRIC MODELING OF AN ELECTRICAL TEST RIG FOR POWER OPTIMIZED AIRCRAFT ARCHITECTURES |
ICAS2008-6.6 ST (AIAA 2008-8973) |
6. Systems, Subsystems and Equipments |
| ALTERNATIVE ENERGY BASED SYSTEMS FOR ADVANCED U.A.V.; THE “SAVE” PROJECT |
ICAS2008-6.6 ST: |
6. Systems, Subsystems and Equipments |
| A PROGRAM OF AIRCRAFT EQUIPMENT AND SUBSYSTEMS LIFE EXTENSION |
ICAS2008-P6.1 |
6. Systems, Subsystems and Equipments |
| THE LOW DOWN – DIGITAL TERRAIN DATA FOR AUTOMATIC GROUND COLLISION AVOIDANCE |
ICAS2008-P6.10 |
6. Systems, Subsystems and Equipments |
| ATTITUDE ACCURACY IMPROVEMENT OF ULTRA LOW-GRADE MEMS INS USING ALIGNMENT OF GPS ANNTENA |
ICAS2008-P6.11 |
6. Systems, Subsystems and Equipments |
| DEVELOPMENT AND TEST OF AN INTEGRATED SENSOR SYSTEM FOR AUTONOMOUS COLLISION AVOIDANCE |
ICAS2008-P6.12 |
6. Systems, Subsystems and Equipments |
| THE NUMERICAL SIMULATION ANALYSIS OF KEY STRUCTURES OF INTEGRATED POWER SUPPLY IN MOTOR-PUMP |
ICAS2008-P6.2 |
6. Systems, Subsystems and Equipments |
| TEST DATA MANAGEMENT FOR AIRCRAFT HYDRAULIC SYSTEM TESTING |
ICAS2008-P6.3 |
6. Systems, Subsystems and Equipments |
| FLIGHT EVALUATION OF A COMPACT AIRBORNE TRACE GAS ANALYSIS SENSOR PROOF-OF-CONCEPT |
ICAS2008-P6.4 |
6. Systems, Subsystems and Equipments |
| ERGONOMIC ASSESSMENT METHOD FOR COCKPIT LAYOUT OF CIVIL AIRCRAFT X BASED ON VIRTUAL DESIGN |
ICAS2008-P6.5 |
6. Systems, Subsystems and Equipments |
| DESIGN AND OPERATION OF THE ADD ENVIRONMENTAL TEST FACILITY |
ICAS2008-P6.6 |
6. Systems, Subsystems and Equipments |
| THE SIGNAL-TO-NOISE RATIO MODELING OF RADAR IN ELECTRONIC COUNTER-COUNTER MEASURES |
ICAS2008-P6.7 |
6. Systems, Subsystems and Equipments |
| LANDING-AVIONIC SYSTEM FOR SMALL-MEDIUM AIRCRAFT FOR AUTOMATED LANDING ON SMALL-MEDIUM AND/OR POORLY EQUIPPED AIRPORTS |
ICAS2008-P6.8 |
6. Systems, Subsystems and Equipments |
| MULTI-DISCIPLINARY INSTALLATION OF THE EAGLE'S EYE |
ICAS2008-P6.9 |
6. Systems, Subsystems and Equipments |
| KNOWLEDGE BASED ENGINEERING TO SUPPORT AIRCRAFT MULTIDISCIPLINARY DESIGN AND OPTIMISATION |
ICAS 2008-6.10.1 |
7. Systems Engineering an Supply Chain |
| SYSTEM INFRASTRUCTURE FOR INTEGRATED AND COLLABORATIVE PRODUCT DEVELOPMENT IN THE AERONAUTIC INDUSTRY |
ICAS 2008-6.10.2 |
7. Systems Engineering an Supply Chain |
| AUTOMATING THE DEVELOPMENT PROCESS OF THERMOPLASTIC COMPOSITE SHEET RIBS USING KNOWLEDGE BASED ENG. TECHNIQUES |
ICAS 2008-6.10.3 |
7. Systems Engineering an Supply Chain |
| DEVELOPMENT AND IMPLEMENTATION OF KNOWLEDGE-BASED DESIGN PROCESS PRIMITIVES |
ICAS 2008-6.10.4 |
7. Systems Engineering an Supply Chain |
| METHODOLOGY OPTIMIZATION OF METAL CUTTING PROGRAMMING APPLIED TO AERONAUTICAL COMPONENTS |
ICAS 2008-6.10.5 |
7. Systems Engineering an Supply Chain |
| FLEET MANAGEMENT SYSTEM FOR AN ADVANCED HELICOPTER PLATFORM - DESIGN & DEVELOPMENT REQUIREMENTS |
ICAS 2008-6.11.1 |
7. Systems Engineering an Supply Chain |
| EVALUATION OF AN INTEROPERABLE VERTICAL TAKE-OFF UAV FOR OPERATIONS WITH UGVS - AN OVERVIEW |
ICAS 2008-6.11.2 |
7. Systems Engineering an Supply Chain |
| KNOWLEDGE MANAGEMENT FOR THROUGH LIFE SUPPORT |
ICAS 2008-6.11.3 |
7. Systems Engineering an Supply Chain |
| LEAN PRODUCT DEVELOPMENT IN THE AEROSPACE ENTERPRISE |
ICAS 2008-6.7.1 |
7. Systems Engineering an Supply Chain |
| F/A 18 E/F TOTAL PRODUCTION SYSTEM |
ICAS 2008-6.7.2 |
7. Systems Engineering an Supply Chain |
| USING LEAN PRINCIPLES AND MBE IN DESIGN AND DEVELOPMENT OF AVIONICS EQUIPMENT AT ROCKWELL COLLINS |
ICAS 2008-6.7.3 |
7. Systems Engineering an Supply Chain |
| DESIGN FOR PROCESS EXCELLENCE - ENSURING TIMELY AND COST EFFECTIVE SOLUTIONS |
ICAS 2008-6.7.4 |
7. Systems Engineering an Supply Chain |
| APPLICATION OF THE INTEGRATED PRODUCT TEAM (IPT) CONCEPT TO THE RE-ENGINE OF A VERY LIGHT JET (VLJ) |
ICAS 2008-6.7.5 |
7. Systems Engineering an Supply Chain |
| DAMAGE TOLERANT FLIGHT CONTROL SYSTEMS FOR UNMANNED AIRCRAFT |
ICAS 2008-6.8.1 INVITED |
7. Systems Engineering an Supply Chain |
| POTENTIAL ACTIVE-VISION CONTROL SYSTEMS FOR UNMANNED AIRCRAFT |
ICAS 2008-6.8.2 INVITED |
7. Systems Engineering an Supply Chain |
| PERSPECTIVES ON (MULTI-) UAV OPERATIONS: AUTONOMY & SECURITY ISSUES |
ICAS 2008-6.8.3 INVITED |
7. Systems Engineering an Supply Chain |
| EUROPE'S RESEARCH TACKLES THE GLOBAL CHALLENGES TO AERONAUTICS |
ICAS 2008-6.9.1 INVITED |
7. Systems Engineering an Supply Chain |
| THE REGIONAL AEROSPACE CLUSTER POLICY IN EUROPE |
ICAS 2008-6.9.2 |
7. Systems Engineering an Supply Chain |
| KEY EXAMPLES AND POTENTIAL OF AVIATION YOUTH PROGRAMS IN GERMANY |
ICAS 2008-6.9.3 |
7. Systems Engineering an Supply Chain |
| FRAMEWORK OF PAKISTAN AEROSPACE INDUSTRY QUALITY SYSTEM |
ICAS 2008-6.9.4 |
7. Systems Engineering an Supply Chain |
| ADVANCED MANUFACTURING GRID SUPPORTING AVIATION INDUSTRY EXTENSIVE COLLABORATIVE DESIGN AND SIMULATION |
ICAS2008-6.10 ST: |
7. Systems Engineering an Supply Chain |
| NUMERICAL SIMULATION OF FORMING PROCESS OF AIRCRAFT TRANSPARENCIES MANUFACTURED BY POLYMERIC PLATE |
ICAS2008-P7.1 |
7. Systems Engineering an Supply Chain |
| MDO DESIGN SUPPORT BY INTEGRATED ENGINEERING SERVICES WITHIN A MULTI-AGENT TASK ENVIRONMENT |
ICAS 2008-1.11.1 (AIAA 2008-8947) |
8. Air Transport System Efficiency |
| A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET |
ICAS 2008-1.11.2 (AIAA 2008-8948) |
8. Air Transport System Efficiency |
| DEVELOPMENT OF A LANDING DRAG CHUTE SYSTEM SYSTEM FOR VERY LIGHT JETS |
ICAS 2008-1.11.3 (AIAA 2008-8950) |
8. Air Transport System Efficiency |
| AIRSHIP TRANSPORT OPERATIONAL MANAGEMENT IN NORTHERN LATITUDES |
ICAS 2008-10.1.1 (AIAA 2008-8850) |
8. Air Transport System Efficiency |
| LOW COST TRANS-RIVER AERIAL-FERRY USING A NOVEL LTA SYSTEM |
ICAS 2008-10.1.2 (AIAA 2008-8851) |
8. Air Transport System Efficiency |
| DESIGN, FABRICATION AND OPERATION OF REMOTELY CONTROLLED AIRSHIPS IN INDIA |
ICAS 2008-10.1.3 (AIAA 2008-8853) |
8. Air Transport System Efficiency |
| TOWARDS SESAR PERFORMANCE TARGETS - THE SUPER-HIGHWAY APPROACH |
ICAS 2008-10.10.1 (AIAA 2008-8935) |
8. Air Transport System Efficiency |
| CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS |
ICAS 2008-10.10.2 (AIAA 2008-8936) |
8. Air Transport System Efficiency |
| IMPACT OF US-EU OPEN AREA AVIATION TREATY ON US AVIATION: A PARAMETRIC ANALYSIS WITH SIMULATION |
ICAS 2008-10.10.3 (AIAA 2008-8937) |
8. Air Transport System Efficiency |
| ON-DEMAND SPECIAL USE AIRSPACE |
ICAS 2008-10.10.4 (AIAA 2008-8938) |
8. Air Transport System Efficiency |
| PRINCIPLES OF AIRSPACE TUBE DESIGN FOR DYNAMIC AIRSPACE CONFIGURATION |
ICAS 2008-10.10.5 (AIAA 2008-8939) |
8. Air Transport System Efficiency |
| FLY AROUND THE WORLD WITH A SOLAR POWERED AIRPLANE |
ICAS 2008-10.11.1 (AIAA 2008-8954 ) |
8. Air Transport System Efficiency |
| MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT |
ICAS 2008-10.11.2 (AIAA 2008-8956) |
8. Air Transport System Efficiency |
| A NEW APPROACH TO FORCED FLAPPING FOR THE ORNICOPTER |
ICAS 2008-10.11.3 (AIAA 2008-8975) |
8. Air Transport System Efficiency |
| AUTOMATED ASSEMBLY TIME ANALYSIS USING A DIGITAL KNOWLEDGE BASED APPROACH |
ICAS 2008-10.3.1 (AIAA 2008-8861) |
8. Air Transport System Efficiency |
| USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY |
ICAS 2008-10.3.2 (AIAA 2008-8862) |
8. Air Transport System Efficiency |
| 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) |
8. Air Transport System Efficiency |
| DESIGN OF A LEAN MRO BUSINESS PROCESS FOR EPCOR |
ICAS 2008-10.3.4 (AIAA 2008-8864) |
8. Air Transport System Efficiency |
| TOWARD AN ECONOMIC MODEL TO INCENTIVIZE VOLUNTARY OPTIMIZATION OF NAS TRAFFIC FLOW |
ICAS 2008-10.4.1 (AIAA 2008-8887) |
8. Air Transport System Efficiency |
| ANALYSIS OF INTERACTION BETWEEN AIR TRANSPORTATION AND ECONOMIC ACTIVITY |
ICAS 2008-10.4.2 (AIAA 2008-8888) |
8. Air Transport System Efficiency |
| DEMAND-CENTRIC ANALYSIS OF THE AIR TRANSPORTATION SYSTEM |
ICAS 2008-10.4.3 (AIAA 2008-8889) |
8. Air Transport System Efficiency |
| NETWORK AND ENVIRONMENTAL IMPACTS OF PASSENGER AND AIRLINE RESPONSE TO COST AND DELAY |
ICAS 2008-10.4.4 (AIAA 2008-8890) |
8. Air Transport System Efficiency |
| EVALUATION OF ANCHORAGE INTERNATIONAL AIRPORT USING THE AIRPORT BUSINESS SUITE |
ICAS 2008-10.4.5 (AIAA 2008-8891) |
8. Air Transport System Efficiency |
| SAY WHO? PILOTED SIMULATION STUDY OF COMMUNICATIONS CENTERED AROUND A COCKPIT TRAFFIC DISPLAY |
ICAS 2008-10.5.1 (AIAA 2008-8895) |
8. Air Transport System Efficiency |
| PILOT IN-TRAIL PROCEDURE VALIDATION SIMULATION STUDY |
ICAS 2008-10.5.2 (AIAA 2008-8896) |
8. Air Transport System Efficiency |
| AN AUTOMATED SIMULATION PILOT CAPABILITY TO SUPPORT ADVANCED AIR TRAFFIC CONTROLLER TRAINING |
ICAS 2008-10.5.3 (AIAA 2008-8897) |
8. Air Transport System Efficiency |
| CONCURRENT AIRCRAFT DESIGN AND RESOURCE ALLOCATION UNDER UNCERTAINTY FOR ON-DEMAND AIR TRANSPORTATION |
ICAS 2008-10.6.1 (AIAA 2008-8903) |
8. Air Transport System Efficiency |
| AEROSPACE PRODUCT COST MANAGEMENT AT THE EARLY CONCEPT OPERATIONS PHASE |
ICAS 2008-10.6.2 (AIAA 2008-8904) |
8. Air Transport System Efficiency |
| MULTI-OBJECTIVE AIRCRAFT OPTIMIZATION FOR MINIMUM COST AND EMISSIONS OVER SPECIFIC ROUTE NETWORKS |
ICAS 2008-10.6.3 (AIAA 2008-8905) |
8. Air Transport System Efficiency |
| LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION |
ICAS 2008-10.6.4 (AIAA 2008-8906 ) |
8. Air Transport System Efficiency |
| CAUSALITY ANALYSIS FOR AVIATION WEATHER HAZARDS |
ICAS 2008-10.7.1 (AIAA 2008-8914) |
8. Air Transport System Efficiency |
| AN ATMOSPHERIC SIMULATION SYSTEM FOR AVIATION REQUIREMENTS OVER NORTHERN LATITUDES |
ICAS 2008-10.7.2 (AIAA 2008-8915) |
8. Air Transport System Efficiency |
| ESTIMATION OF AIR TRAFFIC DELAY USING THREE DIMENSIONAL WEATHER INFORMATION |
ICAS 2008-10.7.3 (AIAA 2008-8916) |
8. Air Transport System Efficiency |
| METHODOLOGIES FOR ESTIMATING THE IMPACT OF SEVERE WEATHER ON AIRSPACE CAPACITY |
ICAS 2008-10.7.4 (AIAA 2008-8917) |
8. Air Transport System Efficiency |
| OPERATIONAL ASSESSMENT OF THE INTEGRATED TERMINAL WEATHER SYSTEM (ITWS) USING DIRECT MEASUREMENT |
ICAS 2008-10.7.5 (AIAA 2008-8918) |
8. Air Transport System Efficiency |
| DEVELOPMENT AND APPLICATION OF AN INTEGRATED APPROACH TOWARD NASA AIRSPACE SYSTEMS RESEARCH |
ICAS 2008-10.8.1 (AIAA 2008-8924) |
8. Air Transport System Efficiency |
| NEXTGEN AND SESAR: OPPORTUNITIES FOR UAS INTEGRATION |
ICAS 2008-10.8.2 (AIAA 2008-8925) |
8. Air Transport System Efficiency |
| PERFORMANCE-BASED TMA HANDLING FOR MIXED TRAFFIC USING A GROUND BASED 4D-GUIDANCE FOR UNEQUIPPED AIRCRAFT |
ICAS 2008-10.8.3 |
8. Air Transport System Efficiency |
| TRAJECTORY UNCERTAINTY MODELING FOR QUEUEING ANALYSIS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.1.1 (AIAA 2008-8854) |
8. Air Transport System Efficiency |
| MODELLING AIRLINE ROUTING AND SCHEDULING UNDER AIRPORT CAPACITY CONSTRAINTS |
ICAS 2008-11.1.2 (AIAA 2008-8855) |
8. Air Transport System Efficiency |
| 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) |
8. Air Transport System Efficiency |
| INTEGRATED TIME-BASED FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.10.1 (AIAA 2008-8940) |
8. Air Transport System Efficiency |
| ANALYSIS OF GAPS BETWEEN THE PREDICTIVE AND THE ADAPTIVE COMPONENT IN ATM |
ICAS 2008-11.10.2 (AIAA 2008-8941) |
8. Air Transport System Efficiency |
| QUEUEING NETWORK MODELS OF THE NATIONAL AIRSPACE SYSTEM |
ICAS 2008-11.10.3 (AIAA 2008-8942) |
8. Air Transport System Efficiency |
| CONTROLLER SUPPORT FOR MANAGING HIGH-EFFICIENCY ARRIVALS IN DENSE TRAFFIC ENVIRONMENTS |
ICAS 2008-11.10.4 (AIAA 2008-8943) |
8. Air Transport System Efficiency |
| UTILIZATION OF NETWORK THEORY FOR THE ENHANCEMENT OF ATO AIR ROUTE FORECAST |
ICAS 2008-11.10.5 (AIAA 2008-8944) |
8. Air Transport System Efficiency |
| DEPARTURE TAXI TIME PREDICTIONS USING ASDE-X SURVEILLANCE DATA |
ICAS 2008-11.11.1 (AIAA 2008-8958) |
8. Air Transport System Efficiency |
| SIMULATOR EVALUATION OF A NOVEL SURFACE MOVEMENT AWARENESS AND ALERTING SYSTEM (SMAAS) FOR RUNWAY INCURSION AVOIDANCE |
ICAS 2008-11.11.2 (AIAA 2008-8959) |
8. Air Transport System Efficiency |
| IMPLICATION OF VARIABILITY IN AIRPORT SURFACE OPERATIONS ON 4-D TRAJECTORY PLANNING |
ICAS 2008-11.11.3 (AIAA 2008-8960) |
8. Air Transport System Efficiency |
| SIMPLIFIED METHODS FOR ASSESSING THE IMPACT OF FUEL ENERGY CONTENT ON PAYLOAD-RANGE |
ICAS 2008-11.2.1 (AIAA 2008-8857) |
8. Air Transport System Efficiency |
| SIMULTANEOUS IMPROVEMENTS IN ENVIRONMENTAL PERFORMANCE AND OPERATIONAL EFFICIENCY ENABLED BY SIGNIFICANTLY QUIETER AIRCRAFT |
ICAS 2008-11.2.2 (AIAA 2008-8858) |
8. Air Transport System Efficiency |
| DEFINITION AND DEMONSTRATION OF THE AIRCRAFT PERFORMANCE EVALUATION CAPABILITIES (APECS) TOOL |
ICAS 2008-11.2.3 (AIAA 2008-8859) |
8. Air Transport System Efficiency |
| USING AIRSPACEANALYZER TO EFFICIENTLY PROVIDE SPACING FOR AIRCRAFT ACROSS MULTIPLE SECTORS |
ICAS 2008-11.2.4 (AIAA 2008-8860 ) |
8. Air Transport System Efficiency |
| ANALYSIS OF LATERAL FLIGHT INEFFICIENCY IN GLOBAL AIR TRAFFIC MANAGEMENT |
ICAS 2008-11.3.1 (AIAA 2008-8865) |
8. Air Transport System Efficiency |
| INTERDEPENDENCIES IN LOCAL AIR QUALITY AND NOISE IMPACTS FOR LANDING AND TAKEOFF OPERATIONS |
ICAS 2008-11.3.2 (AIAA 2008-8866) |
8. Air Transport System Efficiency |
| HIERARCHICAL AND SENSITIVITY ANALYSIS FOR NOISE ABATEMENT DEPARTURE PROCEDURES |
ICAS 2008-11.3.3 (AIAA 2008-8867) |
8. Air Transport System Efficiency |
| TAILORED ARRIVALS OPERATIONS AT SFO AND EXPECTED ENVIRONMENTAL BENEFITS |
ICAS 2008-11.3.4 (AIAA 2008-8868) |
8. Air Transport System Efficiency |
| SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS |
ICAS 2008-11.4.1 (AIAA 2008-8881) |
8. Air Transport System Efficiency |
| IMPACT OF PREDICTION UNCERTAINTY ON THE SAFETY PERFORMANCE OF AIRBORNE SEPARATION |
ICAS 2008-11.4.2 (AIAA 2008-8882) |
8. Air Transport System Efficiency |
| A SYSTEM SAFETY FRAMEWORK FOR ANALYZING FUTURE AIR TRANSPORTATION SEPARATION ASSURANCE AND COLLISION AVOIDANCE CONCEPTS |
ICAS 2008-11.4.3 (AIAA 2008-8883) |
8. Air Transport System Efficiency |
| A PERFORMANCE ASSESSMENT OF A TACTICAL AIRBORNE SEPARATION ASSISTANCE SYSTEM USING REALISTIC, COMPLEX TRAFFIC FLOWS |
ICAS 2008-11.4.4 (AIAA 2008-8884) |
8. Air Transport System Efficiency |
| HUMAN-IN-THE-LOOP EVALUATION OF GROUND-BASED AUTOMATED SEPARATION ASSURANCE FOR NEXTGEN |
ICAS 2008-11.4.5 (AIAA 2008-8885) |
8. Air Transport System Efficiency |
| AIRSPACE SECURITY MEASURES EMPLOYED FOR THE UN GENERAL ASSEMBLY MEETING: ANALYSIS AND IMPACT |
ICAS 2008-11.5.1 (AIAA 2008-8892) |
8. Air Transport System Efficiency |
| SECURE AIRSPACE: A CRITICAL COMPONENT OF NEXTGEN'S LAYERED, ADAPTIVE SECURITY |
ICAS 2008-11.5.2 (AIAA 2008-8893) |
8. Air Transport System Efficiency |
| SECURITY OF WIRELESS SENSOR NETWORK ENABLED HEALTH MONITORING FOR FUTURE AIRPLANES |
ICAS 2008-11.5.3 (AIAA 2008-8894) |
8. Air Transport System Efficiency |
| OPERATIONAL IMPROVEMENTS FROM IN-TRAIL PROCEDURE IN THE NORTH ATLANTIC ORGANIZED TRACK SYSTEM |
ICAS 2008-11.6.1 (AIAA 2008-8898) |
8. Air Transport System Efficiency |
| MULTI-OBJECTIVE OPTIMIZATION OF USER PREFERRED 4D TRAJECTORIES IN THE NAS |
ICAS 2008-11.6.2 (AIAA 2008-8899) |
8. Air Transport System Efficiency |
| MODIFIED BEZIER CURVE FOR 4D REFERENCE TRAJECTORY DEFINITION UNDER FLIGHT PROFILE CONSTRAINT |
ICAS 2008-11.6.3 (AIAA 2008-8900) |
8. Air Transport System Efficiency |
| FLIGHT DECK PROCEDURAL GUIDELINES FOR DATALINK TRAJECTORY NEGOTIATIONS |
ICAS 2008-11.6.4 (AIAA 2008-8901) |
8. Air Transport System Efficiency |
| MODEL-BASED AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.1 (AIAA 2008-8907) |
8. Air Transport System Efficiency |
| AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-11.7.2 (AIAA 2008-8908) |
8. Air Transport System Efficiency |
| TASK ANALYSIS FOR FEASIBILITY ASSESSMENT OF A COLLABORATIVE TRAFFIC FLOW MANAGEMENT CONCEPT |
ICAS 2008-11.7.3 (AIAA 2008-8909) |
8. Air Transport System Efficiency |
| SOLVING HIGH-FIDELITY, LARGE-SCALE TRAFFIC FLOW MANAGEMENT PROBLEMS IN REDUCED TIME |
ICAS 2008-11.7.4 (AIAA 2008-8910) |
8. Air Transport System Efficiency |
| COLLABORATIVE FLOW MANAGEMENT: ANALYSIS OF BENEFITS DURING CONVECTIVE WEATHER DISRUPTIONS |
ICAS 2008-11.7.5 (AIAA 2008-8911) |
8. Air Transport System Efficiency |
| IMPROVED PREDICTION OF GATE DEPARTURE TIMES USING PRE-DEPARTURE EVENTS |
ICAS 2008-11.8.1 (AIAA 2008-8919) |
8. Air Transport System Efficiency |
| BENEFIT POTENTIAL OF CONTINUOUS CLIMB AND DESCENT OPERATIONS |
ICAS 2008-11.8.2 (AIAA 2008-8920) |
8. Air Transport System Efficiency |
| AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION FOR TAKE-OFF AND DEPARTURE |
ICAS 2008-11.8.3 (AIAA 2008-8921) |
8. Air Transport System Efficiency |
| TERMINAL AREA REQUIRED TIME OF ARRIVAL (RTA) CONCEPT OF OPERATIONS AND AUTOMATION PROTOTYPE |
ICAS 2008-11.9.1 (AIAA 2008-8930) |
8. Air Transport System Efficiency |
| SIMULATION RESULTS FOR AIRBORNE PRECISION SPACING ALONG CONTINUOUS DESCENT ARRIVALS |
ICAS 2008-11.9.2 (AIAA 2008-8931) |
8. Air Transport System Efficiency |
| ANALYSIS OF ARRIVAL MANAGEMENT PERFORMANCE WITH AIRCRAFT REQUIRED TIME OF ARRIVAL CAPABILITIES |
ICAS 2008-11.9.3 (AIAA 2008-8932) |
8. Air Transport System Efficiency |
| IMPACT OF ESTOL CAPABILITY ON RUNWAY CAPACITY - AN ANALYTICAL APPROACH |
ICAS 2008-11.9.4 (AIAA 2008-8933) |
8. Air Transport System Efficiency |
| REAL TIME SIMULATION OF INTEGRATION OF UAV'S INTO AIRSPACE |
ICAS 2008-8.1.1 |
8. Air Transport System Efficiency |
| NATIONAL TECHNOLOGY PROJECT 'OUTCAST' ON UAV SENSE AND AVOID |
ICAS 2008-8.1.2 |
8. Air Transport System Efficiency |
| LARGE UAS OPERATIONS IN THE NAS - THE NASA 2007 WESTERN STATES FIRE MISSIONS |
ICAS 2008-8.1.3 (AIAA 2008-8967) |
8. Air Transport System Efficiency |
| AUTOMATED SEPARATION ASSURANCE IN THE PRESENCE OF UNCERTAINTY |
ICAS 2008-8.11.1 |
8. Air Transport System Efficiency |
| PERFORMANCE OF THE WAKE VORTEX PREDICTION AND MONITORING SYSTEM WSVBS AT FRANKFURT AIRPORT |
ICAS 2008-8.11.2 |
8. Air Transport System Efficiency |
| INFORMATION REQUIREMENTS FOR SUPERVISORY AIR TRAFFIC CONTROLLERS IN SUPPORT OF A MID-TERM WAKE VORTEX DEPARTURE SYSTEM |
ICAS 2008-8.11.3 |
8. Air Transport System Efficiency |
| CONTRACT-BASED AIR TRANSPORTATION SYSTEM TO FULFILL THE ARRIVING-ON-TIME OBJECTIVE |
ICAS 2008-8.2.1 |
8. Air Transport System Efficiency |
| PREDICTION OF WEATHER-RELATED DELAYS IN THE CONTINENTAL UNITED STATES |
ICAS 2008-8.2.2 |
8. Air Transport System Efficiency |
| RELATIONSHIP OF MAXIMUM MANAGEABLE AIR TRAFFIC CONTROL COMPLEXITY AND SECTOR CAPACITY |
ICAS 2008-8.2.3 |
8. Air Transport System Efficiency |
| HARMONIZING AUTOMATION, PILOT AND AIR TRAFFIC CONTROLLER IN THE FUTURE AIR TRAFFIC MANAGEMENT |
ICAS 2008-8.2.4 |
8. Air Transport System Efficiency |
| AUGMENTED VISION VIDEOPANORAMA SYSTEM FOR REMOTE AIRPORT TOWER OPERATION |
ICAS 2008-8.3.1 |
8. Air Transport System Efficiency |
| OPERATIONAL CONCEPT FOR AN AIRPORT OPERATIONS CENTER TO ENABLE TOTAL AIRPORT MANAGEMENT |
ICAS 2008-8.3.2 |
8. Air Transport System Efficiency |
| AIRLINES’ POINT OF VIEW AS A NEW APPROACH TO MEASURING QUALITY OF SERVICE AT AIRPORTS |
ICAS 2008-8.3.3 |
8. Air Transport System Efficiency |
| A METHODOLOGICAL APPROACH FOR AIRPORT TECHNOLOGY EVALUATION AND SELECTION |
ICAS 2008-8.3.4 (AIAA 2008-8965) |
8. Air Transport System Efficiency |
| SYSTEM OF SYSTEMS DESIGN FOR WORLDWIDE COMMERCIAL AIRCRAFT NETWORKS |
ICAS 2008-8.4.1 |
8. Air Transport System Efficiency |
| A HOLISTIC APPROACH TO EVALUATE THE AIR TRANSPORTATION SYSTEM |
ICAS 2008-8.4.2 |
8. Air Transport System Efficiency |
| IMPLEMENTING NEXT GENERATION AIR TRANSPORTATION SYSTEM TECHNOLOGIES |
ICAS 2008-8.4.3 |
8. Air Transport System Efficiency |
| PREDICTIVE MODELS OF THE NATIONAL AIRSPACE SYSTEM USING BAYESIAN NETWORKS |
ICAS 2008-8.4.4 |
8. Air Transport System Efficiency |
| INNOVATIVE FUTURE AIR TRANSPORT SYSTEM: SIMULATION OF A FULLY AUTOMATED ATS |
ICAS 2008-8.4.5 |
8. Air Transport System Efficiency |
| A PRACTICAL APPROACH TO MULTI-OBJECTIVE CAPACITY ANALYSIS OF AN ENVIRONMENT-AWARE AIRPORT |
ICAS 2008-8.5.1 |
8. Air Transport System Efficiency |
| PRELIMINARY GUIDELINES ON FLIGHT DECK PROCEDURES FOR VERY CLOSELY SPACED PARALLEL APPROACHES |
ICAS 2008-8.5.2 |
8. Air Transport System Efficiency |
| CAPACITY RESEARCH OF BRNO-TURANY AIRPORT WITH RESPECT TO NEW TRENDS IN AIR TRANSPORT |
ICAS 2008-8.5.3 |
8. Air Transport System Efficiency |
| AN OPTIMIZATION MODEL FOR REDUCING AIRCRAFT TAXI TIMES AT THE DALLAS-FORT WORTH INTERNATIONAL AIRPORT |
ICAS 2008-8.6.1 |
8. Air Transport System Efficiency |
| NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE |
ICAS 2008-8.6.2 |
8. Air Transport System Efficiency |
| AN INTEGRATED USER-ORIENTED WEATHER FORECAST SYSTEM FOR AIR TRAFFIC USING REAL-TIME OBSERVATIONS AND MODEL DATA |
ICAS 2008-8.6.3 |
8. Air Transport System Efficiency |
| BASE OF OPERATIONS CONCEPT FOR ON-DEMAND OPERATIONS |
ICAS 2008-8.6.4 (AIAA 2008-8977 ) |
8. Air Transport System Efficiency |
| PERFORMANCE BASIS FOR AIRBORNE SEPARATION |
ICAS 2008-8.7.1 |
8. Air Transport System Efficiency |
| ASSESSMENT OF FLIGHT CREW ACCEPTANCE OF AUTOMATED RESOLUTION SUGGESTIONS AND MANUAL RESOLUTION TOOLS |
ICAS 2008-8.7.2 |
8. Air Transport System Efficiency |
| REAL-TIME SIMULATION OF A DISTRIBUTED CONFLICT RESOLUTION ALGORITHM |
ICAS 2008-8.7.3 |
8. Air Transport System Efficiency |
| A SYSTEMATIC PROCEDURE FOR DETERMINING SEPARATION MINIMA |
ICAS 2008-8.7.4 |
8. Air Transport System Efficiency |
| ALGORITHM AND OPERATIONAL CONCEPT FOR RESOLVING SHORT-RANGE CONFLICTS |
ICAS 2008-8.7.5 |
8. Air Transport System Efficiency |
| NETWORK ENABLED OPERATIONS ENHANCES AVIATION EFFICIENCY |
ICAS 2008-8.8.1 (AIAA 2008-8951) |
8. Air Transport System Efficiency |
| CAPACITY MODELLING FOR FUTURE AERONAUTICAL SAFETY COMMUNICATIONS OVER WIDE AREAS |
ICAS 2008-8.8.2 (AIAA 2008-8952) |
8. Air Transport System Efficiency |
| PRELIMINARY ANALYSIS OF STRATEGIES AND CHALLENGES TO ENCOURAGE DATA LINK ADOPTION OVER THE NORTH ATLANTIC AIRSPACE |
ICAS 2008-8.8.3 (AIAA 2008-8953) |
8. Air Transport System Efficiency |
| AUTOMATED CONFLICT RESOLUTION - A SIMULATION-BASED SENSITIVITY STUDY OF AIRSPACE AND DEMAND |
ICAS 2008-8.9.1 |
8. Air Transport System Efficiency |
| ENABLING TECHNOLOGY EVALUATION FOR EFFICIENT CONTINUOUS DESCENT APPROACHES |
ICAS 2008-8.9.2 |
8. Air Transport System Efficiency |
| DEFINING DYNAMIC CRITICAL POINTS FOR DYNAMIC AIRSPACE CONFIGURATION |
ICAS 2008-8.9.3 |
8. Air Transport System Efficiency |
| DESIGN OF OPERATION DATABASE FOR ATM PERFORMANCE ASSESSMENT |
ICAS 2008-8.9.4 |
8. Air Transport System Efficiency |
| DESIGN ANALYSIS OF AN AIRCRAFT PARACHUTE RECOVERY SYSTEM FOR VERY LIGHT JETS |
ICAS2008-1.11 ST (AIAA 2008-8949) |
8. Air Transport System Efficiency |
| THE MODERNIZED NATIONAL AIRSPACE SYSTEM PERFORMANCE ANALYSIS CAPABILITY (NASPAC) |
ICAS 2008-9.11.2 (AIAA 2008-8945) |
8. Air Transport System Efficiency |
| AN ONTOLOGY FOR TRAFFIC FLOW MANAGEMENT |
ICAS 2008-9.11.1 (AIAA 2008-8946) |
8. Air Transport System Efficiency |
| MICROSCOPIC ANALYSIS OF AIRPORT SURFACE SEQUENCING |
ICAS2008-11.11 ST (AIAA 2008-8961) |
8. Air Transport System Efficiency |
| TACTICAL CONFLICT RESOLUTION USING VERTICAL MANEUVERS IN ENROUTE AIRSPACE |
ICAS2008-11.4 ST (AIAA 2008-8886) |
8. Air Transport System Efficiency |
| RAPID PREDICTION OF AIR TRAFFIC FOR TRAJECTORY BASED OPERATIONS |
ICAS2008-11.6 ST (AIAA 2008-8902) |
8. Air Transport System Efficiency |
| NATSIM: A SYSTEMS DYNAMICS MODEL OF NORTH ATLANTIC AIR TRAFFIC |
ICAS 2008-9.11.3 (AIAA 2008-8912) |
8. Air Transport System Efficiency |
| OPERATIONAL ACCEPTABILITY OF ISSUING RNAV/RNP PROCEDURE CHANGES IN FUTURE TERMINAL ENVIRONMENTS |
ICAS2008-11.8 ST (AIAA 2008-8922) |
8. Air Transport System Efficiency |
| GENERATION OF HIGH ACCURATE 4D TRAJECTORIES FOR TAKE-OFF AND DEPARTURE |
ICAS2008-8.11 ST: |
8. Air Transport System Efficiency |
| TOWARDS 4D TRAJECTORY MANAGEMENT: CONTAINMENT AND THE USE OF RNP IN CONSTRAINED TERMINAL AIRSPACE |
ICAS2008-8.11 ST: |
8. Air Transport System Efficiency |
| A NOVEL APPROACH TO AIR TRANSPORT SYSTEM ENVIRONMENTAL IMPACT EVALUATION THROUGH PHYSICAL MODELLING AND SIMULATION |
ICAS2008-8.3 ST: |
8. Air Transport System Efficiency |
| THE USE OF MODELS FOR ATM VALIDATION: FROM AIRPORT EXTENSION PROGRAMS TO THE AIR TRANSPORT SYSTEM OF THE FUTURE |
ICAS2008-8.9 ST: |
8. Air Transport System Efficiency |
| VISAGE - A NEW VISION FOR GEOSPATIAL DATA VISUALIZATION AND ANALYSIS |
ICAS2008-P8.1 (AIAA 2008-8872) |
8. Air Transport System Efficiency |
| DESIGN AND DEVELOPMENT OF AN ATC DISTRIBUTED TRAINING SYSTEM |
ICAS2008-P8.2 (AIAA 2008-8873) |
8. Air Transport System Efficiency |
| FROM ANALOGUE BROADCAST RADIO TOWARDS END-TO-END COMMUNICATION |
ICAS2008-P8.3 (AIAA 2008-8874) |
8. Air Transport System Efficiency |
| AN APPROACH FOR VERIFICATION AND VALIDATION OF THE ENVIRONMENTAL DESIGN SPACE |
ICAS2008-P8.4 (AIAA 2008-8875) |
8. Air Transport System Efficiency |
| SECURITY ARCHITECTURE AND FORMAL ANALYSIS OF AN AIRPLANE SOFTWARE DISTRIBUTION SYSTEM |
ICAS 2008-9.1.1 |
9. Safety and Security |
| THREAT ASSESSMENT AND RESPONSE MANAGEMENT SYSTEM TARMS: AN ON-BOARD AIRCRAFT SECURITY SYSTEM |
ICAS 2008-9.1.2 |
9. Safety and Security |
| SECURITY OF WIRELESS SENSOR NETWORK ENABLED HEALTH MONITORING FOR FUTURE AIRPLANES |
ICAS 2008-9.1.3 |
9. Safety and Security |
| RESEARCH ON INTEGRATED COLLIMATED COCKPIT VISUAL AND FLIGHT INFORMATION SYSTEM |
ICAS 2008-9.10.1 |
9. Safety and Security |
| DESIGN OF EXPERIMENT FOR THE PILOT EVALUATION OF AN AIRBORNE RUNWAY INCURSION ALERTING SYSTEM |
ICAS 2008-9.10.2 |
9. Safety and Security |
| DESIGN AND EVALUATION OF A 4D INTERFACE FOR ATC |
ICAS 2008-9.10.3 |
9. Safety and Security |
| BIOMECHANICAL PILOT PROPERTIES IDENTIFICATION BY INVERSE KINEMATICS/INVERSE DYNAMICS MULTIBODY ANALYSIS |
ICAS 2008-9.10.4 |
9. Safety and Security |
| THE SIMULATION OF THE HUMAN-MACHINE PARTNERSHIP IN UCAV OPERATION |
ICAS 2008-9.10.5 |
9. Safety and Security |
| CBAQ: DEVELOPMENT OF CRM BEHAVIOR ANALYSIS METHOD FOR MISSION FLIGHT CREW TRAINING |
ICAS 2008-9.2.1 |
9. Safety and Security |
| AVIATION TELEMEDICINE: PAST, PRESENT AND FUTURE |
ICAS 2008-9.2.2 |
9. Safety and Security |
| IDENTIFYING FATIGUE OF FLIGHT ATTENDANTS IN SHORT-HAUL OPERATIONS |
ICAS 2008-9.2.3 |
9. Safety and Security |
| THE IMPLEMENTATION OF ANALYTICAL HIERARCHY PROCESS IN FLIGHT SAFETY |
ICAS 2008-9.2.4 |
9. Safety and Security |
| A PROGNOSTIC METHOD TO IDENTIFY HAZARDS FOR FUTURE AVIATION CONCEPTS |
ICAS 2008-9.3.1 |
9. Safety and Security |
| A SIMULATION BENCHMARK FOR AIRCRAFT SURVIVABILITY ASSESSMENT |
ICAS 2008-9.3.2 |
9. Safety and Security |
| ADVANCED METHODOLOGIES FOR AVERAGE PROBABILITY CALCULATION FOR AEROSPACE SYSTEMS |
ICAS 2008-9.3.3 |
9. Safety and Security |
| FLIGHT SAFETY AS CONSIDERED IN PROBABILISTIC TERMS |
ICAS 2008-9.3.4 |
9. Safety and Security |
| 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 ) |
9. Safety and Security |
| THE IMPACT OF RIGOROUS METHODS ON AERONAUTICAL REGULATIONS |
ICAS 2008-9.7.1 |
9. Safety and Security |
| HAZARD, SAFETY RISK AND UNCERTAINTY MODELING OF THE INTEGRATION OF UNMANNED AIRCRAFT SYSTEMS INTO THE NATIONAL AIRSPACE |
ICAS 2008-9.7.2 |
9. Safety and Security |
| THE SAFETY GAINED BY EQUIPMENT AND PROCEDURES USED TO PERFORM CONSTANT ANGLE APPROACHES |
ICAS 2008-9.7.3 |
9. Safety and Security |
| COMPARING SITUATION AWARENESS MEASUREMENT TECHNIQUES IN A LOW FIDELITY AIR TRAFFIC CONTROL SIMULATION |
ICAS 2008-9.7.4 |
9. Safety and Security |
| A MODEL FOR ESTIMATING THE LATERAL OVERLAP PROBABILITY OF AIRCRAFT WITH RNP ALERTING CAPABILITY IN PARALLEL RNAV ROUTES |
ICAS 2008-9.7.5 |
9. Safety and Security |
| PILOTED SIMULATION RESULTS OF AN ONBOARD WAKE VORTEX DETECTION, WARNING AND AVOIDANCE SYSTEM AND COCKPIT DISPLAY ASPECTS |
ICAS 2008-9.9.1 |
9. Safety and Security |
| DEVELOPMENT OF AN ONBOARD DOPPLER LIDAR FOR FLIGHT SAFETY |
ICAS 2008-9.9.2 |
9. Safety and Security |
| WAKE TURBULENCE MITIGATION FOR ARRIVALS (WTMA) |
ICAS 2008-9.9.3 |
9. Safety and Security |
| ON THE PROBABILITY OF COLLISION FOR CLIMBING AND DESCENDING TRAJECTORIES RELEVANT TO AIR TRAFFIC MANAGEMENT |
ICAS2008-9.3 ST: |
9. Safety and Security |
| SAFE AUTOMATIC FLIGHT BACK AND LANDING OF AIRCRAFT (SOFIA) |
ICAS2008-9.7 ST: |
9. Safety and Security |
| ADAPTING THE ACCIMAP FOR AN ANALYSIS OF THE SQ006 ACCIDENT |
ICAS2008-P9.1 (AIAA 2008-8878) |
9. Safety and Security |
| THE SYSTEM FAULT BEHAVIOR AND MODEL |
ICAS2008-P9.2 |
9. Safety and Security |
| COORDINATELY MODELING AND SIMULATION OF THE EJECTION SEAT/OCCUPANT SYSTEM |
ICAS2008-P9.3 |
9. Safety and Security |
| ASSESSMENT OF THE POTENTIAL OF HYDROGEN FUELED LARGE LONG-RANGE TRANSPORT AIRCRAFT |
ICAS 2008-1.2.4 |
10. Challenge of the Environment |
| ACHIEVING HIGHLY EFFICIENT CIVIL AVIATION - WHY & HOW WITH AIR-TO-AIR REFUELLING, REVIEW & NEW DEVELOPMENTS |
ICAS 2008-4.10.1 |
10. Challenge of the Environment |
| COMBINATORIAL OPTIMIZATION TO INCLUDE GREENER TECHNOLOGIES IN A SHORT-TO-MEDIUM RANGE COMMERCIAL AIRCRAFT |
ICAS 2008-4.10.2 (AIAA 2008-8963) |
10. Challenge of the Environment |
| THE GREEN FREIGHTER PROJECT - OBJECTIVES AND FIRST RESULTS |
ICAS 2008-4.10.3 |
10. Challenge of the Environment |
| NOVEL DESIGN CONCEPTS FOR AIRCRAFT WITH REDUCED NOISE AND GLOBAL WARMING CHARACTERISTICS |
ICAS 2008-4.10.4 |
10. Challenge of the Environment |
| A GREEN ALTERNATIVE FOR PILOT TRAINING |
ICAS 2008-4.10.5 |
10. Challenge of the Environment |
| OPTIMIZATION OF RNAV NOISE ABATEMENT ARRIVAL TRAJECTORIES |
ICAS 2008-4.11.1 |
10. Challenge of the Environment |
| ENVIRONMENT-AWARE RUNWAY ALLOCATION ADVICE SYSTEM |
ICAS 2008-4.11.2 |
10. Challenge of the Environment |
| TECHNOLOGY-ENABLED IMPROVEMENTS FOR TERMINAL AREA CAPACITY AND ENVIRONMENTAL IMPACT |
ICAS 2008-4.11.3 |
10. Challenge of the Environment |
| AIRBUS: TOWARDS AN ECO-EFFICIENT ENTERPRISE |
ICAS 2008-4.7.1 INVITED |
10. Challenge of the Environment |
| GOING GREEN – MITIGATING AVIATION’S NEW ENVIRONMENTAL DRIVERS |
ICAS 2008-4.7.2 |
10. Challenge of the Environment |
| THE ENVIRONMENTAL DESIGN SPACE |
ICAS 2008-4.7.3 |
10. Challenge of the Environment |
| PAYLOAD FUEL ENERGY EFFICIENCY AS A METRIC FOR AVIATION ENVIRONMENTAL PERFORMANCE |
ICAS 2008-4.7.4 |
10. Challenge of the Environment |
| THE FEASIBILITY AND POTENTIAL ENVIRONMENTAL BENEFITS OF ALTERNATIVE FUELS FOR COMMERCIAL AVIATION |
ICAS 2008-4.7.5 |
10. Challenge of the Environment |
| EVALUATION OF SIMULATOR AND FLIGHT TESTED NOISE ABATEMENT APPROACH PROCEDURES |
ICAS 2008-4.8.1 |
10. Challenge of the Environment |
| DESIGN OF 4D LANDING APPROACH TRAJECTORIES FOR A QUIET STOL AIRPLANE |
ICAS 2008-4.8.2 |
10. Challenge of the Environment |
| NOISE REDUCTION BY THRUST VECTORING FOR SUPERSONIC BUSINESS JET |
ICAS 2008-4.8.3 |
10. Challenge of the Environment |
| ENVIRONMENTALLY PROGRESSIVE AIRPLANES THROUGH AN INTEGRATED DESIGN FOR INTERIOR NOISE |
ICAS 2008-4.9.1 INVITED |
10. Challenge of the Environment |
| PIEZO ACTIVE VIBRATION AND NOISE CONTROL IN HELICOPTERS |
ICAS 2008-4.9.2 INVITED |
10. Challenge of the Environment |
| A NOVEL RECIPROCAL SOUND TRANSMISSION MEASURING METHOD, APPLIED ON A COMPOSITE FUSELAGE |
ICAS 2008-4.9.3 |
10. Challenge of the Environment |
| PROBLEMS OF VIBROACOUSTICS FOR NEW AIRPLANE GENERATION |
ICAS 2008-4.9.4 |
10. Challenge of the Environment |
| TRENDS IN GLOBAL NOISE AND EMISSIONS FROM COMMERCIAL AVIATION FOR 2000 THROUGH 2025 |
ICAS2008-4.7 ST: |
10. Challenge of the Environment |
| ON THE REDUCTION OF NOX-EMISSION LEVELS BY PERFORMING LOW NOX FLIGHTS |
ICAS2008-4.7 ST: |
10. Challenge of the Environment |
| EFFECT OF ATMOSPHERIC PROPAGATION ON AIRCRAFT NOISE |
ICAS2008-P10.1 |
10. Challenge of the Environment |
| A METHOD FOR ASSESSING THE ENVIRONMENTAL BENEFIT OF FUTURE AVIATION TECHNOLOGIES |
ICAS2008-P10.2 |
10. Challenge of the Environment |