ICAS 2006: TOPICS AND TITLES


General Lectures


1. Aircraft and Systems Integration
2. Aerodynamics
3. Materials and Structures
4. Propulsion
5. Flight Dynamics and Control
6. Systems, Subsystems and Equipments
7. Systems Engineering an Supply Chain
8. Air Transport System Efficiency
9. Safety and Security
10. Challenge of the Environment


DEVELOPMENTS IN FLIGHT GUIDANCE AND CONTROL , ICAS 2006-0.1: ICAS DANIEL & FLORENCE GUGGENHEIM MEMORIAL LECTURE: INVITED:

General Lecture

THE A380 PROGRAMME, ICAS 2006-0.6: VON KARMAN LECTURE: INVITED: (approved draft)

General Lecture

DESIGN OF THE BLENDED-WING-BODY SUBSONIC TRANSPORT , ICAS 2006-0.7: LUDWIG BÖLKOW LECTURE:

General Lecture

DISTRIBUTED ON-DEMAND AIR TRANSPORTATION USING SMALL AIRPLANES AND SMALL AND UNDERUTILIZED COMMUNITY AIRPORTS , ICAS 2006-0.5: GENERAL LECTURE IV: INVITED:

General Lecture

KEY TECHNOLOGY ENABLERS FOR THE FUTURE OF AERONAUTICAL EQUIPMENT INDUSTRY , ICAS 2006-0.2: GENERAL LECTURE I: INVITED:

General Lecture

THE EDUCATION OF FUTURE AERONAUTICAL ENGINEERS: CONCEIVING, DESIGNING, IMPLEMENTING AND OPERATING , ICAS 2006-0.4: GENERAL LECTURE III: INVITED:

General Lecture

THE INTERNATIONAL DEVELOPMENT AND PRODUCTION OF THE F2-FIGHTER , ICAS 2006-0.3: GENERAL LECTURE II: INVITED:

General Lecture

A BRAZILIAN EXPERIENCE IN TEACHING AIRCRAFT DESIGN , ICAS 2006-P1.4

1. Aircraft and Systems Integration

A COMPARATIVE STUDY OF FOUR UCAV WING LAYOUTS - HIGH SPEED AERO PERFORMANCE & STABILITY CONSIDERATIONS , ICAS 2006-1.7.2

1. Aircraft and Systems Integration

A COMPARISON OF EMPIRICAL AND CFD-BASED EXERGY MODELLING FOR THE AIRFRAME SUBSYSTEM OF AIRCRAFT DESIGN , ICAS 2006-1.9.2

1. Aircraft and Systems Integration

A HYBRID GENETIC/LNTERIOR-POINT ALGORITHM FOR MULTI-DISCIPLINARY OPTIMIZATION PROBLEMS IN AIRCRAFT PRELIMINARY DESIGN, ICAS 2006-1.11.1

1. Aircraft and Systems Integration

A METHODOLOGY FOR TECHNOLOGY EVALUATION AND CAPABILITY TRADEOFF FOR COMPLEX SYSTEM ARCHITECTURES , ICAS 2006-1.2.1

1. Aircraft and Systems Integration

A MORPHING UAV WITH ROTARY AND FIXED-WING MODES , ICAS 2006-1.10.5

1. Aircraft and Systems Integration

A NEW METHOD FOR OPTIMUM ALLOCATION OF DESIGN REQUIREMENTS IN AIRCRAFT CONCEPTUAL DESIGN , ICAS2006-1.11S

1. Aircraft and Systems Integration

A POWERED LIFT DESIGN FOR SUBSONIC CIVIL TRANSPORT AIRCRAFT , ICAS2006-1.3S

1. Aircraft and Systems Integration

A PRACTICAL MULTIDISCIPLINARY DESIGN OPTIMIZATION ALGORITHM BASED ON THE UNIFORM DESIGN THEORY , ICAS2006-1.9S

1. Aircraft and Systems Integration

A VIRTUAL ENVIRONMENT, DISTRIBUTED SIMULATION, UAV TESTBED , ICAS2006-1.10S

1. Aircraft and Systems Integration

AERODYNAMIC PERFORMANCE OF A BLENDED-WING-BODY CONFIGURATION AIRCRAFT , ICAS 2006-1.6.2

1. Aircraft and Systems Integration

AN ENHANCED SCENARIO APPROACH ASSESSING UNCERTAINTIES IN THE REALIZATION OF NEW AIRCRAFT AND TECHNOLOGIES , ICAS 2006-1.9.1

1. Aircraft and Systems Integration

AN INTEGRATED AND GENERIC VULNERABILITY ASSESSMENT SYSTEM FOR AIRCRAFT NONNUCLEAR SURVIVABILITY DESIGN , ICAS 2006-1.2.4

1. Aircraft and Systems Integration

AN INTEGRATED PLATFORM FOR AIRCRAFT DESIGN: FLIGHT ENGINEERING SIMULATOR , ICAS 2006-P1.1

1. Aircraft and Systems Integration

AN INTEGRATED SYSTEM FOR BORDER SURVEILLANCE AND MONITORING BASED ON VERY LIGHT MALE UAV , ICAS 2006-1.7.5

1. Aircraft and Systems Integration

AN INTELLIGENT, KNOWLEDGE-BASED MULTI-CRITERIA DECISION MAKING ADVISOR FOR AEROSPACE SYSTEMS DESIGN , ICAS 2006-1.9.3

1. Aircraft and Systems Integration

AN OVERVIEW OF AIRCRAFT MECHANICS AND STRUCTURES , ICAS 2006-1.5.1

1. Aircraft and Systems Integration

APPLICATION OF THE VARIABLE-FIDELITY MDO TOOLS TO A JET AIRCRAFT DESIGN , ICAS 2006-1.8.1

1. Aircraft and Systems Integration

AUTOMATION OF CONCEPTUAL DESIGN OF VERTICAL TAKE-OFF UAVS – DEMONSTRATION MODEL , ICAS 2006-1.10.1

1. Aircraft and Systems Integration

CONCEPTUAL DESIGN OF ROADABLE AIRCRAFT , ICAS 2006-1.4.5

1. Aircraft and Systems Integration

DESIGN AND TESTING OF A MODEL WING SECTION FOR A HUMAN POWERED AIRCRAFT , ICAS 2006-P1.2

1. Aircraft and Systems Integration

DESIGN APPROACH FOR A VERTICAL TAKE-OFF UNMANNED AERIAL VEHICLE WITH INTEROPERABLE CAPABILITIES – PAYLOAD ISSUES , ICAS2006-1.10S

1. Aircraft and Systems Integration

DESIGN TRENDS FOR ROTARY-WING UNMANNED AIR VEHICLES , ICAS 2006-1.10.2

1. Aircraft and Systems Integration

DESIGN, ANALYSIS, FABRICATION AND FLIGHT TEST VALIDATION OF THE NWPU25 MICRO AIR VEHICLE , ICAS 2006-1.10.3

1. Aircraft and Systems Integration

DEVELOPMENT AND FLIGHT TESTING OF AN AUTONOMOUS PARAFOIL-LOAD SYSTEM DEMONSTRATOR , ICAS 2006-1.1.3

1. Aircraft and Systems Integration

DEVELOPMENT OF AN MAV MANEUVERED BY SHIFTING THE LOCATION OF CENTER OF GRAVITY , ICAS 2006-1.10.4

1. Aircraft and Systems Integration

DEVELOPMENT OF EXPERIMENTAL SMALL UAV EQUIPPED WITH CELLULAR PHONE DATA LINK SYSTEM , ICAS2006-1.7S

1. Aircraft and Systems Integration

DISTRIBUTED PROPULSION FEASIBILITY STUDIES , ICAS 2006-1.3.2

1. Aircraft and Systems Integration

EDUCATIONAL FLIGHT TESTING, ICAS 2006-1.5.2

1. Aircraft and Systems Integration

ELECTRIC POWERED COMMUTER AIRCRAFT, ICAS2006-1.6S

1. Aircraft and Systems Integration

EUROPEAN ACTIVITIES FOR CIVIL UAV APPLICATIONS , ICAS 2006-1.7.1

1. Aircraft and Systems Integration

EVOLUTIONAL DESIGN SUPPORT STRATEGY ORIENTED TO AIRCRAFT CONCEPTUAL DESIGN , ICAS2006-1.2S

1. Aircraft and Systems Integration

FIRST RESULTS OF THE 2ND FLIGHT TEST CAMPAIGN USING AN AIRBUS A 340 IN THE EUROPEAN AWIATOR PROJECT ON WING TECHNOLOGIES, ICAS 2006-1.3.1

1. Aircraft and Systems Integration

FITTING FITNESS IN AIRCRAFT DESIGN , ICAS 2006-1.11.3

1. Aircraft and Systems Integration

FLAVIIR, AN INNOVATIVE UNIVERSITY / INDUSTRY RESEARCH PROGRAM FOR COLLABORATIVE RESEARCH & DEMONSTRATION OF UAV TECHNOLOGIES , ICAS 2006-1.1.2

1. Aircraft and Systems Integration

HYDROGEN FUELLED LARGE LONG RANGE TRANSPORT AIRCRAFT, ICAS 2006-1.4.3

1. Aircraft and Systems Integration

INTEGRATION OF DESIGN TO SUPPORT AS PART OF AIRCRAFT DEVELOPMENT , ICAS 2006-1.8.3

1. Aircraft and Systems Integration

LOCAL PARETO ANALYSER FOR PRELIMINARY DESIGN , ICAS 2006-1.11.2

1. Aircraft and Systems Integration

LOW COST, FLEXIBLE PLATFORM FOR IN SITU REMOTE SENSING , ICAS 2006-1.1.1

1. Aircraft and Systems Integration

MULTIOBJECTIVE OPTIMIZATION OF ENGINE & A/C MATCHING ON MISSION AND ENVIRONMENTAL CRITERIA AT SSBJ CONCEPTUAL DESIGN, ICAS2006-1.4S

1. Aircraft and Systems Integration

MULTIOBJECTIVE EVOLUTIONARY ALGORITHMS APPLIED TO AIRCRAFT ENGINE DESIGN , ICAS 2006-1.8.2

1. Aircraft and Systems Integration

National Experimental Supersonic Transport Project , ICAS 2006-1.4.1 INVITED:

1. Aircraft and Systems Integration

NOVEL CONCEPTS FOR AIRCRAFT COMPONENT TECHNOLOGIES: THE NACRE EUROPEAN INTEGRATED PROJECT, ICAS 2006-1.6.1

1. Aircraft and Systems Integration

ON THE DESIGN OPTIMIZATION OF A THRUST-VECTORED HIGH-SUBSONIC JET TRANSPORT AIRCRAFT, ICAS2006-1.4S

1. Aircraft and Systems Integration

OPTIMISING TRANSPORT FLYING WINGS , ICAS 2006-1.6.3

1. Aircraft and Systems Integration

PRELIMINARY DESIGN OF A RANGE OF HYDROGEN-POWERED CIVIL TRANSPORT AIRCRAFT, ICAS 2006-1.4.4

1. Aircraft and Systems Integration

PULSED PLASMA PROPULSION AND FLOW CONTROL FOR BIONIC AIRSHIPS, ICAS2006-1.6S

1. Aircraft and Systems Integration

RE-ANALYSIS OF A MULTI-MISSION RE-CONFIGURABLE UAV – REVISED DESIGN CONCEPT , ICAS 2006-1.7.4

1. Aircraft and Systems Integration

REPETITIVE RESPONSE SURFACE ENHANCEMENT TECHNIQUE THROUGH DESIGN SPACE TRANSFORMATION AND SUB-OPTIMIZATION, ICAS2006-1.9S

1. Aircraft and Systems Integration

REPRESENTATION OF STRUCTURAL SOLUTIONS IN BLENDED WING BODY PRELIMINARY DESIGN , ICAS 2006-1.6.4

1. Aircraft and Systems Integration

SILENT SUPERSONIC TECHNOLOGY DEMONSTRATION PROGRAM , ICAS 2006-1.4.2

1. Aircraft and Systems Integration

STUDY ON DECISION CONFLICT OF UAV SYSTEM , ICAS 2006-P1.3

1. Aircraft and Systems Integration

STUDY ON DESIGN AND TRANSITIONAL FLIGHT OF TAIL-SITTING VTOL UAV , ICAS 2006-1.7.3

1. Aircraft and Systems Integration

SURVIVABILITY EVALUATION AND SUSTAINABLE DEVELOPABILITY INTEGRATED TRADEOFF METHODS FOR MILITARY AIRCRAFT , ICAS 2006-1.2.2

1. Aircraft and Systems Integration

THE DESIGN OF A HIGH-MANEUVERABLE SINGLE- MINI-JET ENGINED REMOTELY PILOTED VEHICLE (RPV), ICAS2006-1.1S

1. Aircraft and Systems Integration

THE INVESTIGATION OF CYCLOGYRO DESIGN AND THE PERFORMANCE , ICAS 2006-1.3.3

1. Aircraft and Systems Integration

THE RESEARCH OF STRUCTURAL OPTIMIZATION WITH THE CONSTRAINTS OF AERODYNAMICS AND RADAR CROSS SECTION (RCS) OF AIRCRAFT , ICAS 2006-1.9.4

1. Aircraft and Systems Integration

TRANSPORT AIRCRAFT RESEARCH CHALLENGES – DLR-ONERA PARTNERSHIP , ICAS 2006-1.3.4

1. Aircraft and Systems Integration

USING INFORMATION ENTROPY TO ASSESS AIRCRAFT SIGNATURES INTEGRATED EFFECT , ICAS 2006-1.2.3

1. Aircraft and Systems Integration

A BEST PRACTICES SYSTEM FOR REDUCED UNCERTAINTY IN CFD , ICAS 2006-2.6.1

2. Aerodynamics

A CFD ANALYSIS OF THE 14-BIS AIRCRAFT AERODYNAMICS , ICAS 2006-2.2.2

2. Aerodynamics

A COUPLED PRESCRIBED WAKE-EULER SOLVER FOR EFFICIENT COMPUTING HELICOPTER ROTOR FLOWS IN HOVER , ICAS 2006-2.2.4

2. Aerodynamics

A NEW APPROACH IN CFD SUPPORTED WIND TUNNEL TESTING , ICAS 2006-3.4.2

2. Aerodynamics

A STUDY OF NONLINEAR EDDY-VISCOSITY MODELS IN A FLOW SOLVER FOR TURBOMACHINERY , ICAS 2006-2.5.2

2. Aerodynamics

A STUDY ON AERODYNAMIC DESIGN INTEGRATION OF THE SUPERCRITICAL WING AND REAR-MOUNTED ENGINE CONFIGURATION , ICAS 2006-P2.5

2. Aerodynamics

A VARIABLE FIDELITY OPTIMIZATION FRAMEWORK USING SECOND-ORDER, MULTI-POINT, ADDITIVE SCALING FUNCTIONS APPLIED TO AIRFOIL DESIGN , ICAS 2006-P2.17

2. Aerodynamics

ACTIVE CONTROL OF SEPARATION ON TWO AND THREE DIMENSIONAL HIGH-LIFT CONFIGURATIONS , ICAS 2006-3.5.1

2. Aerodynamics

ADAPTIVE LOAD REDISTRIBUTION USING MINI-TEDS , ICAS 2006-3.9.1

2. Aerodynamics

AERODYNAMIC COEFFICIENT PREDICTION OF A GENERAL TRANSPORT AIRCRAFT USING NEURAL NETWORK , ICAS 2006-2.6.3

2. Aerodynamics

AERODYNAMIC DESIGN FOR WING-BODY BLENDED AND INLET , ICAS 2006-P2.16

2. Aerodynamics

AERODYNAMIC EFFICIENCY STUDY OF MODERN SPIROID WINGLETS , ICAS2006-3.7S

2. Aerodynamics

AERODYNAMIC MODELING USING FLIGHT MECHANICAL SIMULATIONS, FLIGHT TESTS AND OPTIMIZATION , ICAS 2006-3.10.3

2. Aerodynamics

AERODYNAMIC SHAPE OPTIMIZATION OF TRANSONIC AIRFOIL AND WING USING RESPONSE SURFACE METHODOLOGY , ICAS 2006-2.1.3

2. Aerodynamics

AERODYNAMIC SHAPE OPTIMIZATION OF UNGUIDED PROJECTILES USING ANT COLONY OPTIMIZATION AND GENETIC ALGORITHM , ICAS2006-3.6S

2. Aerodynamics

AERODYNAMIC STUDY OF A BLENDED WING BODY; COMPARISON WITH A CONVENTIONAL TRANSPORT AIRPLANE , ICAS 2006-P2.8

2. Aerodynamics

AERODYNAMIC STUDY OF HIGH-LIFT DEVICE CONFIGURATIONS FOR TAKE-OFF AND LANDING CONDITIONS , ICAS 2006-2.3.2

2. Aerodynamics

AEROLOADS. A TOOL TO GENERATE PRESSURE LOAD MODELS OF AN AIRCRAFT FITTED TO AN AERODYNAMIC DATA BASE, ICAS2006-3.9S

2. Aerodynamics

AIAA CFD DRAG PREDICTION WORKSHOP: AN OVERVIEW , ICAS 2006-2.4.1

2. Aerodynamics

AIRBRAKE INDUCED FIN BUFFET LOADS ON FIGHTER AIRCRAFT , ICAS 2006-3.9.2

2. Aerodynamics

AIRFOIL DESIGN OF TAILLESS UNMANNED AIR VEHICLE (UAV) , ICAS 2006-P2.7

2. Aerodynamics

AN EFFICIENT PRECONDITIONING METHOD AND ITS APPLICATION TO NUMERICAL SIMULATION OF STEADY AND UNSTEADY VISCOUS FLOWS , ICAS 2006-2.6.4

2. Aerodynamics

AN EXPERIMENTAL AND ANALYTICAL INVESTIGATION OF AERODYNAMIC FLOW CONTROL USING SYNTHETIC JET TECHNOLOGY , ICAS 2006-P2.3

2. Aerodynamics

ANALYTICAL SOLUTION OF THE EULER EQUATIONS FOR AIRFOIL FLOW AT SUBSONIC AND TRANSONIC CONDITIONS , ICAS 2006-2.4.4

2. Aerodynamics

ANGLE-OF-ATTACK IMPACT ON THE AEROTHERMODYNAMIC PERFORMANCE OF FLAT-NOSE POWER-LAW BODIES IN HYPERSONIC AIRFLOW , ICAS 2006-2.7.3

2. Aerodynamics

APPLICATION OF ADVANCED SURFACE SENSORS FOR THE DETECTION AND CONTROL OF FLOW SEPARATION ON AN INDUSTRIAL HIGH-LIFT CONFIGURATION , ICAS 2006-2.11.3

2. Aerodynamics

APPLICATIONS OF DIFFERENT MEASURING TECHNIQUES FOR TRANSITION DETECTION IN LOW AND HIGH SPEED FLIGHT EXPERIMENTS , ICAS 2006-3.3.1

2. Aerodynamics

BOUNDARY-LAYER CONTROL BY BLOWING AT THE TEST-SECTION OF A LOW-SPEED WIND TUNNEL , ICAS 2006-3.4.3

2. Aerodynamics

COMPUTATION OF EQUIVALENT ACOUSTIC SOURCES USING AN INVERSE METHOD, ICAS 2006-P2.23

2. Aerodynamics

COMPUTATIONAL ANALYSES OF SUPERSONIC FLOWS OVER A DELTA WING AT HIGH ANGLES OF ATTACK , ICAS2006-2.5S

2. Aerodynamics

COMPUTATIONAL INVESTIGATION OF THE FLIR POD INTERFERENCE EFFECTS ON THE CF-18 AIRCRAFT STORES, ICAS 2006-2.2.1

2. Aerodynamics

COMPUTATIONAL AEROACOUSTIC PREDICTION OF TRANSONIC ROTOR NOISE BASED ON REYNOLDS-AVERAGED N-S FLOW SIMULATION , ICAS 2006-2.10.3

2. Aerodynamics

COMPUTATIONAL AERODYNAMIC ANALYSIS ON A GENERIC UCAV/URAV CONFIGURATION , ICAS2006-2.2S

2. Aerodynamics

COMPUTATIONAL AERODYNAMIC BEHAVIOUR OF LOCATION AND INCLINATION OF LATERAL  PLATE /JET-  INTERACTIONS WITH HYPERSONIC FLOWFIELD , ICAS2006-2.7S

2. Aerodynamics

CONIC CURVE DESCRIPTION OF FLAPPING WING PLANFORMS AND PARAMETRIC INVESTIGATION OF THEIR PERFORMANCE, ICAS2006-3.10S

2. Aerodynamics

COST-EFFICIENT USE OF PARALLEL COMPUTERS IN AIRCRAFT DESIGN , ICAS 2006-2.6.2

2. Aerodynamics

DECAY CHARACTERISTICS OF SINGLE AND DOUBLE WAKE-VORTEX PAIRS IN DIFFERENT ATMOSPHERIC FLOW REALISATIONS , ICAS 2006-3.8.1

2. Aerodynamics

DESIGN FOR SPIN , ICAS 2006-3.11.2

2. Aerodynamics

DEVELOPMENT OF A NEW BOUNDARY LAYER CONTROL TECHNIQUE FOR AUTOMOTIVE WIND TUNNEL TESTING , ICAS 2006-3.5.3

2. Aerodynamics

DIRECT MEASUREMENT OF WALL-SHEAR STRESS OF PLANE SHEAR LAYER WITH PLASMA SYNTHETIC JET ACTUATOR , ICAS2006-3.5S

2. Aerodynamics

DNW’S METHOD TO CORRECT FOR SUPPORT AND WALL INTERFERENCE EFFECTS ON LOW SPEED MEASUREMENTS WITH A LARGE PROPELLER POWERED TRANSPORT AIRCRAFT MODEL , ICAS 2006-3.4.5

2. Aerodynamics

DUAL-CODE SOLUTION PROCEDURE FOR EQUILIBRIUM HYPERSONIC AXISYMMETRIC TRANSITIONAL/TURBULENT FLOWS , ICAS 2006-2.4.5

2. Aerodynamics

EFFECT OF CENTER-BODY ON THE VORTEX FLOW OF A DELTA WING WITH LEADING EDGE EXTENSION , ICAS 2006-3.1.1

2. Aerodynamics

EFFECTS OF HELICOPTER ROTOR WAKE CHARACTERISTICS ON BLADE AIRLOADS , ICAS 2006-3.8.3

2. Aerodynamics

EULERIAN WATER IMPINGEMENT PREDICTION ON MULTI-ELEMENT AIRFOILS WITH VISCOUS AND INVISCID FLOW, ICAS2006-2.5S

2. Aerodynamics

EXERGY BASED DESIGN METHODOLOGY FOR AIRFOIL SHAPE OPTIMIZATION AND WING ANALYSIS , ICAS2006-3.11S

2. Aerodynamics

EXPERIMENTAL AND NUMERICAL ANALYSIS ON LIFT AND TRANSITION CHARACTERISTICS OF ONERA-M5 CONFIGURATION MODEL , ICAS 2006-2.3.3

2. Aerodynamics

EXPERIMENTAL AND NUMERICAL STUDY OF A TWO-ELEMENT WING WITH GURNEY FLAP , ICAS2006-3.8S

2. Aerodynamics

EXPERIMENTAL RESEARCH OF AERODYNAMICS ON AN SST CONFIGURATION WITH HIGH LIFT DEVICES , ICAS 2006-5.11.3

2. Aerodynamics

EXPERIMENTAL STUDY AND NUMERICAL SIMULATION  OF FLOW AROUND WING CONTROL SURFACE , ICAS 2006-3.6.2

2. Aerodynamics

EXPERIMENTAL STUDY OF CONTAMINATED AIRFOIL WITH FOWLER FLAP , ICAS2006-3.5S

2. Aerodynamics

FLAPPING-WING THRUST IN COMPRESSIBLE FLOW , ICAS 2006-3.10.4

2. Aerodynamics

FLOW SIMULATION OF AN SST CONFIGURATION AT LOW-SPEED AND HIGH-LIFT CONDITIONS , ICAS 2006-3.7.3

2. Aerodynamics

FORCED HEAVE OSCILLATIONS OF A SUPERCRITICAL SWEPT WING IN TRANSONIC FLOW, ICAS 2006-3.2.3

2. Aerodynamics

GEOMETRY MODIFICATIONS OF NONPLANAR WING TIP DESIGN FOR ADAPTATION TO LOW SPEED RANGE , ICAS 2006-3.11.3

2. Aerodynamics

GROUND MOBILE LABORATORY FOR MEASUREMENT OF AIRFOIL AERODYNAMIC CHARACTERISTICS , ICAS2006-3.4S

2. Aerodynamics

HALF MODEL TESTING AND SIDEWALL EFFECTS , ICAS2006-3.4S

2. Aerodynamics

HEAT TRANSFER CHARACTERISTICS OF LITHIUM COOLANT FLOWING THROUGH A CURVED BEND USING MODIFIED TOROIDAL COORDINATE SYSTEM , ICAS 2006-P2.15

2. Aerodynamics

HICON AERODYNAMICS-  HIGH LIFT AERODYNAMIC DESIGN FOR THE FUTURE , ICAS 2006-3.7.5

2. Aerodynamics

IHAAA APPLICATIONS TO STORE SEPARATION , ICAS 2006-P2.9

2. Aerodynamics

IMPACT OF MODEL PLUNGING MOTION ON WIND TUNNEL WALL PRESSURE FLUCTUATIONS , ICAS2006-3.2S

2. Aerodynamics

IMPLEMENTATION OF HIGH-ORDER COMPACT SCHEMES TO THE  ITERATIVE PARABOLIZED NAVIER-STOKES EQUATIONS , ICAS 2006-2.1.2

2. Aerodynamics

INCOMPRESSIBLE NAVIER STOKES EQUATIONS SOLUTION USING BLOCK NESTED CARTESIAN GRID , ICAS2006-2.1S

2. Aerodynamics

INFLUENCE OF CAPTIVE STORES ON THE UNSTEADY PRESSURE DISTRIBUTION WITHIN A RECTANGULAR CAVITY , ICAS 2006-3.9.4

2. Aerodynamics

INITIAL STEADY /  UNSTEADY CFD ANALYSIS OF VORTEX FLOW OVER THE VFE-2 DELTA WING , ICAS 2006-P2.18

2. Aerodynamics

INVESTIGATING ACTIVE VORTEX GENERATORS AS A NOVEL HIGH-LIFT DEVICE , ICAS 2006-3.7.4

2. Aerodynamics

INVESTIGATION OF ERROR SOURCES ON THE BALANCE AND THE STANDARD DYNAMIC MODEL IN THE WIND TUNNEL , ICAS2006-3.2S

2. Aerodynamics

INVESTIGATION OF FLOW PHENOMENA ON GENERIC DELTA WING , ICAS 2006-3.1.2

2. Aerodynamics

INVESTIGATION ON AN ACTIVE WINGLET INFLUENCING THE WAKE OF A LARGE TRANSPORT AIRCRAFT , ICAS 2006-3.8.2

2. Aerodynamics

INVESTIGATIONS OF UNSTEADY FLOW FIELDS IN TRANSONIC WIND TUNNELS USING PARTICLE IMAGE VELOCIMETRY, ICAS 2006-3.2.4

2. Aerodynamics

LAMINAR AIRFOIL MODIFICATION ATTAINING OPTIMUM DRAG REDUCTION BY USE OF AIRFOIL MORPHING , ICAS 2006-2.7.1

2. Aerodynamics

LAMINAR-TURBULENT TRANSITION CORRELATIONS IN SUPERSONIC/ HYPERSONIC FLOW , ICAS 2006-3.6.4

2. Aerodynamics

MODELING AND CONTROL OF A WIRE-DRIVEN PARALLEL SUPPORT SYSTEM WITH LARGE ATTACK ANGLES IN LOW SPEED WIND TUNNELS , ICAS 2006-3.5.2

2. Aerodynamics

MODELLING OF DYNAMIC STABILITY DERIVATIVES USING CFD , ICAS 2006-3.10.5

2. Aerodynamics

MODIFICATION OF DELTA WINGS TO CONTROL VORTEX BREAKDOWN, ICAS 2006-P2.19

2. Aerodynamics

MULTIBODY SIMULATION OF AN AEROELASTIC DELTA WING IN ROLL MANOEUVRES, ICAS 2006-3.10.2

2. Aerodynamics

NEW MEASUREMENT TECHNIQUES IN THE ONERA LARGE WIND TUNNELS , ICAS 2006-3.3.3

2. Aerodynamics

NOISE GENERATION AROUND NACA0012 WINGTIP USING LARGE-EDDY-SIMULATION , ICAS 2006-2.10.1

2. Aerodynamics

NON-LINEAR PHENOMENA ANALYSIS AND CHAOS PREDICTION OF STALL-INDUCED AEROELASTIC OSCILLATIONS VIA LYAPUNOV EXPONENTS , ICAS2006-3.10S

2. Aerodynamics

NUM. AND EXP. INVESTIGATIONS ON THE APPLICATION OF VORTEX GENERATORS FOR SHOCK WAVE-/BOUNDARY LAYER-INTERACTION CONTROL, ICAS 2006-2.9.3

2. Aerodynamics

NUMERICAL ANALYSIS OF FLAPPING WING , ICAS 2006-2.2.3

2. Aerodynamics

NUMERICAL CALCULATION OF CONFINED COAXIAL TURBULENT SWIRLING JETS , ICAS 2006-P2.1

2. Aerodynamics

NUMERICAL COMPUTATION OF THE X-15 WIND TUNNEL AND FLIGHT EXPERIMENTS: A VALIDATION AND VERIFICATION CASE STUDY , ICAS 2006-2.4.3

2. Aerodynamics

NUMERICAL DESIGN AND ASSESSMENT OF A BIPLANE AS FUTURE SUPERSONIC TRANSPORT-  REVISITING  BUSEMANN'S BIPLANE , ICAS 2006-3.7.2

2. Aerodynamics

NUMERICAL INVESTIGATION ON THE AERODYNAMIC EFFECT OF MINI-TEDS ON THE AWIATOR AIRCRAFT CONFIGURATION AT CRUISE CONDITIONS , ICAS 2006-3.9.3

2. Aerodynamics

NUMERICAL SIMULATION OF COMPLEX ICE SHAPES ON SWEPT WINGS , ICAS 2006-2.5.1

2. Aerodynamics

NUMERICAL SIMULATION OF KINETIC EFFECTS IN LOW-DENSITY HYPERSONIC AERODYNAMICS , ICAS 2006-P2.4

2. Aerodynamics

NUMERICAL SIMULATION OF THE FLOWFIELD AROUND MISSILE WITH LATERAL JET INTERACTION , ICAS2006-2.2S

2. Aerodynamics

NUMERICAL SIMULATION OF THIN AIRFOIL STALL BY USING MODIFIED DES APPROACH , ICAS 2006-2.5.3

2. Aerodynamics

NUMERICAL STUDY OF FLOWS IN THE VICINITY OF AIRFOIL TRAILING EDGE , ICAS 2006-2.10.2

2. Aerodynamics

NUMERICAL STUDY OF THE PERFORMACE IMPROVEMENT OF SUBMERGED AIR INTAKES USING VORTEX GENERATORS , ICAS 2006-P2.12

2. Aerodynamics

NUMERICAL STUDY OF EFFECTS OF INJECTION PRESSURE AND LOCATION OF SECONDARY INJECTION INSIDE LOW-THRUST SATELLITE NOZZLE , ICAS 2006-P2.10

2. Aerodynamics

ON IMPROVING STABILITY AND EFFICIENCY OF LU-SGS METHOD FOR INCOMPRESSIBLE VISCOUS FLOWS WITH PSEUDO COMPRESSIBILITY , ICAS 2006-2.1.1

2. Aerodynamics

ON STATUS OF WIND TUNNEL WALL CORRECTION , ICAS 2006-3.4.4

2. Aerodynamics

ON THE CORRELATION OF ACOUSTIC MODES IN A NOZZLE AND IN THE FAR-FIELD , ICAS 2006-2.10.4

2. Aerodynamics

ONE-SHOT PSEUDO-TIMESTEPPING METHOD FOR AERODYNAMIC SHAPE OPTIMIZATION, ICAS2006-2.6S

2. Aerodynamics

ONGOING ACTIVITIES IN FLOW SIMULATION AND SHAPE OPTIMIZATION WITHIN THE GERMAN MEGADESIGN PROJECT , ICAS 2006-3.11.1

2. Aerodynamics

OPTIMIZATION OF THE AFT-BODY GEOMETRY OF AXI-SYMMETRIC SLENDER BODY BASED ON WAVE DRAG CONSIDERATIONS , ICAS 2006-3.6.3

2. Aerodynamics

Performance Testing with High Productivity in a Low Speed Flight Reynolds Number Test Campaign , ICAS 2006-5.11.1

2. Aerodynamics

PIV INVESTIGATION OF AN AIRFOIL WITH A GURNEY FLAP , ICAS 2006-3.1.3

2. Aerodynamics

PIV STUDY OF NEAR WALL ORGANIZED MOTIONS , ICAS 2006-P2.22

2. Aerodynamics

PREDICTION OF HIGH-LIFT SYSTEM AERODYNAMICS USING UNSTRUCTURED-GRID FLOW SOLVERS AND TRANSPORT EQUATION TURBULENCE MODEL, ICAS2006-2.3S

2. Aerodynamics

PREDICTION OF AERODYNAMICS CHARACTERISTICS AND AIRLOADS OF A GENERIC GEOMETRY WING. , ICAS 2006-P2.14

2. Aerodynamics

PRELIMINARY EXPERIMENTS OF FLAPPING WING IN THREE-DEGREE-OF-FREEDOM MOTIONS , ICAS 2006-3.2.2

2. Aerodynamics

PROPULSIVE CHARACTERISTICS OF BIOMORPHING AIRFOILS IN GROUND EFFECT , ICAS2006-2.7S

2. Aerodynamics

RECENT EFFORTS FOR CREDIBLE CFD SIMULATIONS IN CHINA , ICAS 2006-2.4.2

2. Aerodynamics

REYNOLDS NUMBER EFFECTS IDENTIFIED WITH CFD METHODS COMPARED TO SEMI-EMPIRICAL METHODS , ICAS 2006-2.3.4

2. Aerodynamics

ROBUST AIRFOIL OPTIMIZATION BASED ON RESPONSE SURFACE METHOD (RSM), ICAS 2006-P2.6

2. Aerodynamics

SEMI-SPAN TESTING IN WIND TUNNELS , ICAS 2006-3.4.1

2. Aerodynamics

SHEAR CONTROLLED SWIRL JETS BY HELICAL PERTURBATION WAVE , ICAS 2006-P2.2

2. Aerodynamics

SLAT NOISE PREDICTIONS BASED ON APE AND STOCHASTIC SOUND SOURCES FROM  RANS , ICAS 2006-2.8.2

2. Aerodynamics

SMOOTHED PARTICLE HYDRODYNAMICS SIMULATION OF FUEL TANK SLOSHING , ICAS 2006-2.7.4

2. Aerodynamics

SONIC BOOM PREDICTION, FOCUSING AND MITIGATION , ICAS 2006-2.8.3

2. Aerodynamics

STABILIZING A  LAMINAR BOUNDARY-LAYER USING PLASMA-ACTUATORS , ICAS 2006-2.11.2

2. Aerodynamics

SUMMARY OF THE DYNAMIC TEST CAPABILITIES AT CARIA LOW SPEED WIND TUNNEL , ICAS 2006-3.2.1

2. Aerodynamics

SUPERSONIC LAMINAR FLOW CONTROL STUDIES IN THE SUPERTRAC PROJECT , ICAS 2006-2.9.1

2. Aerodynamics

SUPERSONIC/TRANSONIC FLOW CONTROL BY ELECTRO-DISCHARGE PLASMA TECHNIQUE , ICAS 2006-2.11.1

2. Aerodynamics

SURFACE PRESSURE VARIATION ON AN AIRFOIL IN PLUNGING AND PITCHING MOTIONS , ICAS 2006-3.10.1

2. Aerodynamics

THE AC20.30 BLENDED WING BODY CONFIGURATION: DEVELOPMENT & CURRENT STATUS 2006 , ICAS 2006-3.7.1

2. Aerodynamics

THE ANALYSIS OF CYCLOGYRO USING UNSTEADY VORTEX LATTICE METHOD , ICAS 2006-3.6.1

2. Aerodynamics

THE COMPARATIVE EVALUATION OF POWER REQUIREMENTS FOR FIXED, ROTARY AND FLAPPING WINGS  MICRO AIR VEHICLES , ICAS 2006-P2.13

2. Aerodynamics

THE DESIGN OF ADAPTIVE WINGS USING SPINAL STRUCTURES, ICAS 2006-2.7.5

2. Aerodynamics

THE EFFECT OF GEOMETRY ON THE PERFORMANCE OF SYNTHETIC JET ACTUATORS , ICAS 2006-P2.11

2. Aerodynamics

THE HIRENASD PROJECT: HIGH REYNOLDS NUMBER AEROSTRUCTURAL DYNAMICS EXPERIMENTS IN THE EUROPEAN TRANSONIC WINDTUNNEL (ETW) , ICAS 2006-5.11.2

2. Aerodynamics

TRANSITION MEASUREMENT SYSTEM OF EXPERIMENTAL SUPERSONIC TRANSPORT “NEXST-1” , ICAS 2006-3.3.2

2. Aerodynamics

TRENDS FOR LOW NOISE HIGH-LIFT DESIGN DERIVED FROM WIND-TUNNEL TESTS, ICAS 2006-2.8.1

2. Aerodynamics

TURBULENT BOUNDARY LAYER FLOW OVER CIRCULAR CAVITIES , ICAS 2006-2.7.2

2. Aerodynamics

TURBULENT FLOW CONTROL BY ELECTROMAGNETIC FORCES , ICAS 2006-2.9.2

2. Aerodynamics

UNSTEADY AERODYNAMIC ANALYSIS OF WINGS FLYING OVER NONPLANAR GROUND SURFACES, ICAS 2006-P2.20

2. Aerodynamics

USING CRYOTSP AS A TOOL FOR TRANSITION DETECTION, ICAS 2006-3.3.4

2. Aerodynamics

VALIDATION STUDY OF CFD ANALYSIS FOR HIGH-LIFT SYSTEMS , ICAS 2006-2.3.1

2. Aerodynamics

WING ROCK CONTROL VIA EXTERNAL EXCITATION, ICAS 2006-P2.21

2. Aerodynamics

3-D FEM ANALYSIS OF PLASTIC BEHAVIOR INSIDE MMC COMPOSITES CONSIDERING DAMAGE THEORY , ICAS2006-4.9S

3. Materials and Structures

A BREAKTHROUGH IN ASSEMBLY OF AIRCRAFT COMPOSITE STRUCTURES , ICAS 2006-4.4.5

3. Materials and Structures

A GENERALIZED LOCAL STRAIN APPROACH TO CONSIDERING THICKNESS EFFECT ON FATIGUE PERFORMANCE , ICAS2006-4.3S

3. Materials and Structures

A GLOBAL-LOCAL OPTIMIZATION METHOD FOR PROBLEMS IN STRUCTURAL DYNAMICS , ICAS 2006-4.10.4

3. Materials and Structures

A HOLISTIC APPROACH TO FLUTTER CLEARANCE USING CLASSICAL METHODS , ICAS 2006-10.3.4

3. Materials and Structures

A HYBRID WAVE BASED VIBRO-ACOUSTIC MODELLING TECHNIQUE FOR THE PREDICTION OF INTERIOR NOISE IN AN AIRCRAFT FUSELAGE , ICAS 2006-10.1.3

3. Materials and Structures

A MULTIBODY APPROACH FOR MODELLING OF THE MANOEUVRING AEROELASTIC AIRCRAFT DURING PRE-DESIGN , ICAS 2006-10.2.2

3. Materials and Structures

A NEW CONCEPT FOR TESTING FATIGUE AND DAMAGE TOLERANCE AT AEROSPACE STRUCTURE , ICAS 2006-4.2.2

3. Materials and Structures

A NEW TYPE OF LIMIT CYCLE OSCILLATION OCCURRED IN FLUTTER WING MODEL AT TRANSONIC WIND TUNNEL TESTS , ICAS 2006-10.3.2

3. Materials and Structures

A STUDY OF STRUCTURE WEIGHT ESTIMATION FOR HIGH ALTITUDE LONG ENDURANCE (HALE) UNMANNED AERIAL VEHICLE (UAV) , ICAS2006-10.1S

3. Materials and Structures

ACTIVE AEROELASTIC CONTROL OF VARIABLE CAMBER AIRFOIL IN THE PRESENCE OF STRUCTURAL NON-LINEARITIES , ICAS 2006-10.6.1

3. Materials and Structures

ACTUATION CONCEPTS FOR MORPHING HELICOPTER ROTOR BLADES , ICAS 2006-10.6.4

3. Materials and Structures

ADVANCED CONCEPTS FOR NOVEL LANDING GEAR STRUCTURES USING HIGHLY ANISOTROPIC COMPOSITES, ICAS2006-4.10S

3. Materials and Structures

AEROELASTIC ANALYSIS OF TYPICAL SECTIONS WITH STRUCTURAL AND AERODYNAMIC NONLINEARITIES , ICAS2006-10.2S

3. Materials and Structures

AEROELASTIC CONTROL OF A FLEXIBLE WING WITH EMBEDDED PIEZOELECTRIC ACTUATORS, ICAS2006-10.6S

3. Materials and Structures

AGING PREDICTION OF RUBBER ELEMENT BY NEURAL NETWORK , ICAS 2006-P3.3

3. Materials and Structures

AIRCRAFT DITCHING NUMERICAL SIMULATION , ICAS 2006-9.6.2

3. Materials and Structures

AIRCRAFT INTERIOR NOISE REDUCTION THROUGH A PIEZO TUNABLE VIBRATION ABSORBER SYSTEM , ICAS2006-10.1S

3. Materials and Structures

AN ANALYTICAL METHOD IN COMPUTATIONAL AEROELASTICITY BASED ON WAGNER FUNCTION , ICAS2006-10.3S

3. Materials and Structures

AN EXPERIMENTAL STUDY OF THE STRUCTURAL DAMPING OF THE FULL-SCALE HELICOPTER MAIN ROTOR BLADE FROM COMPOSITE LAMINATED MATERIALS , ICAS 2006-10.7.3

3. Materials and Structures

ANALYSIS OF THE STATIC AND DYNAMIC AERO-STRUCTURAL RESPONSE OF AN ELASTIC SWEPT WING MODEL BY DIRECT AEROELASTIC SIMULATION , ICAS 2006-10.3.3

3. Materials and Structures

APPLICATION OF ELECTRIC POTENTIAL METHOD ON MONITORING FATIGUE CRACKING OF AIRCRAFT STRUCTURAL ELEMENTS , ICAS 2006-4.7.4

3. Materials and Structures

ASSESSING THE STRUCTURAL INTEGRITY OF POAF AIRCRAFT , ICAS 2006-P3.9

3. Materials and Structures

BUCKLING AND POST-BUCKLING OF SUB-STIFFENED OR LOCALLY TAILORED ALUMINIUM PANELS , ICAS 2006-10.4.3

3. Materials and Structures

BUCKLING OF WING SPARS UNDER COMBINED LOADING , ICAS2006-10.4S

3. Materials and Structures

CALCULATION OF F/A-18 FATIGUE LOADS AND WING DEFORMATION USING COMPUTATIONAL FLUID DYNAMICS , ICAS 2006-10.5.2

3. Materials and Structures

CHALLENGES OF THE METALLIC FUSELAGE , ICAS 2006-4.5.1

3. Materials and Structures

COMPARATIVE EFFICIENCY OF FINITE ELEMENT MODELS OF CFRP BONDED JOINTS , ICAS 2006-4.11.3

3. Materials and Structures

COMPREHENSIVE DESIGN AND EVALUATION OF AIRCRAFT STRUCTURAL SYSTEM EFFECTIVENESS , ICAS 2006-4.5.3

3. Materials and Structures

COMPUTATIONAL AND EXPERIMENTAL ASSESSMENT OF CONDITIONS FOR CUTTING OF ALLOYED STEEL IN HIGH SPEED MILLING, ICAS2006-4.6S

3. Materials and Structures

COUPLING TECHNIQUES FOR COMPUTATIONAL NONLINEAR TRANSIENT AEROELASTICITY , ICAS 2006-10.2.3

3. Materials and Structures

CRASHWORTHINESS OF AIRCRAFT SEAT , ICAS 2006-P3.13

3. Materials and Structures

CROSS-PLY BENDING AND STABILITY OF COMPRESSED BAR WITH CRACK , ICAS 2006-P3.7

3. Materials and Structures

CYCLIC BUCKLING TESTS OF CFRP CURVED PANELS , ICAS 2006-10.4.5

3. Materials and Structures

DELAMINATION GROWTH RATE AT LOW AND ELEVATED TEMPERATURES IN GLARE , ICAS2006-4.1S

3. Materials and Structures

DESIGN IMPROVEMENT BY SHAPE CHANGE USING A LINEAR FINITE ELEMENT METHOD , ICAS 2006-4.10.2

3. Materials and Structures

DESIGN OF HIGHLY REFLECTIVE TBC SYSTEM FOR GAS TURBINE APPLICATION , ICAS 2006-4.6.3

3. Materials and Structures

DESIGN, OPTIMIS ATION AND TECHNOLOGY OF CARBON COMPOSITE AXIAL FLOW FAN ROTOR BLADE OF LIGHT AIRCRAFT PROPULSION SYSTEM , ICAS2006-4.8S

3. Materials and Structures

DEVELOPMENT AND APPLICATION OF A NEW DESIGN TOOL FOR AEROSPACE STRUCTURES , ICAS 2006-4.10.5

3. Materials and Structures

DEVELOPMENT OF ADVANCED LAMINATES FOR AIRCRAFT STRUCTURES , ICAS 2006-4.1.3

3. Materials and Structures

DEVELOPMENT OF FASTENER MODELS FOR IMPACT SIMULATION OF COMPOSITE STRUCTURES , ICAS2006-10.7S

3. Materials and Structures

DYNAMIC LOADS OF CONTROL SYSTEM ELEMENTS , ICAS2006-10.6S

3. Materials and Structures

DYNAMIC STRENGTH TESTING OF 3D-REINFORCED T-JOINTS , ICAS 2006-4.4.4

3. Materials and Structures

EFFECTS OF GEOMETRY ASPECTS ON THE SIMULATION OF SUPERPLASTICITY IN MMC COMPOSITES , ICAS 2006-P3.12

3. Materials and Structures

EFFICIENT PREDICTION OF COMPOSITE DAMAGE TOLERANCE , ICAS 2006-4.3.2

3. Materials and Structures

EXPERIMENTAL AND NUMERICAL INVESTIGATION ON THE FAILURE MODES OF THICK COMPOSITE LAMINATES , ICAS 2006-4.8.2

3. Materials and Structures

EXPERIMENTAL CONFIRMATION OF LIMIT CYCLE OSCILLATION FOR ACTIVE CONTROL OF TRANSONIC FLUTTER IN WIND TUNNEL , ICAS 2006-10.2.1

3. Materials and Structures

FATIGUE INITIATION  AND CRACK GROWTH BEHAVIOUR IN GLARE FROM THE AIRBUS MEGALINER BARREL TEST , ICAS 2006-4.1.2

3. Materials and Structures

FATIGUE PROPERTIES OF Z-PINNED AIRCRAFT COMPOSITE MATERIALS , ICAS 2006-4.2.3

3. Materials and Structures

FINITE ELEMENT ANALYSIS OF FRICTION STIR WELDING TEMPERATURE FIELD, ICAS 2006-P3.2

3. Materials and Structures

FINITE ELEMENT ANALYSIS FOR THROUGH THICKNESS REINFORCEMENT REPAIR OF DELAMINATED CARBON-EPOXY PANELS , ICAS 2006-4.5.2

3. Materials and Structures

FLUTTER ANALYSIS OF KF-16 AIRCRAFT UTILIZING TEST MODAL DATA , ICAS 2006-P3.8

3. Materials and Structures

FUTURE DESIGN SCENARIO FOR COMPOSITE AIRFRAME PANELS , ICAS 2006-10.4.1

3. Materials and Structures

GLOBAL-LOCAL ANALYSIS OF BONDED SKIN-TO-STIFFENER JOINTS IN POST-BUCKLED PANELS , ICAS 2006-4.11.2

3. Materials and Structures

HEALTH MONITORING OF AIRCRAFT FUSELAGE STRUCTURES USING ULTRASONIC WAVES , ICAS 2006-4.7.3

3. Materials and Structures

HYBRID FABRICATION ROUTE-  COST EFFICIENT CFRP PRIMARY AIRFRAME STRUCTURES , ICAS 2006-4.8.1

3. Materials and Structures

IMPACT DAMAGE MODELLING OF COMPOSITE AEROSPACE STRUCTURES SUBJECT TO BIRD-STRIKE , ICAS 2006-10.7.1

3. Materials and Structures

IMPACT OF BONDED REPAIRS TO CFRP LAMINATES UNDER LOAD , ICAS 2006-4.2.4

3. Materials and Structures

IMPROVEMENT OF THE SOUND TRANSMISSION LOSS OF PANELS BY MEANS OF ACOUSTICALLY TUNED RESONATORS , ICAS 2006-10.1.2

3. Materials and Structures

INERTIA FORCES ROLE IN STATIC AEROELASTICITY , ICAS 2006-10.3.1

3. Materials and Structures

INFLUENCE OF DIFFERENT STIFFENING TYPES OF THE AIRCRAFT BODY STRUCTURE ON THE NOISE EXPOSURE IN THE CABIN , ICAS 2006-10.1.1

3. Materials and Structures

INFLUENCE OF HIGH PERFORMANCE CUTTING OPERATIONS ON THE RESIDUAL STRESSES OF ALUMINUM STRUCTURAL WORKPIECES , ICAS 2006-4.6.4

3. Materials and Structures

INTEGRATED DESIGN OF SMART COMPOSITES APPLIED TO SMART WINGLETS , ICAS 2006-10.6.3

3. Materials and Structures

INTEGRATED VEHICLE HEALTH MANAGEMENT SYSTEMS, ICAS 2006-4.7.1 INVITED:

3. Materials and Structures

INVERSE METHODS FOR DAMAGE IDENTIFICATION IN AERONAUTICAL STRUCTURES, ICAS 2006-4.7.2

3. Materials and Structures

INVESTIGATING AND MODELING OF THE  MULTI-AXIAL FATIGUE AND COMPLEX DEFORMATION OF A NI-BASED SUPERALLOY FOR IMPROVING DISC LIFING , ICAS 2006-4.6.2

3. Materials and Structures

INVESTIGATION OF WAVE PROPAGATION IN COMPOSITES AS REQUIREMENT FOR IMPACT DETECTION , ICAS2006-4.2S

3. Materials and Structures

KOITER’S POSTBUCKLING ANALYSIS OF GENERAL SHELL STRUCTURES USING THE FINITE ELEMENT METHOD , ICAS 2006-4.11.1

3. Materials and Structures

LIQUID COMPOSITE MOULDING FOR AERONAUTICAL STRUCTURES , ICAS 2006-4.4.2

3. Materials and Structures

LQG FLUTTER CONTROL OF WIND TUNNEL MODEL USING PIEZO-CERAMIC ACTUATOR , ICAS 2006-10.6.2

3. Materials and Structures

MAGNESIUM CASTINGS FOR AIRCRAFTS , ICAS 2006-4.9.3

3. Materials and Structures

MATRIX FORMULATION FOR CALCULATIONS OF WING LOADING DISTRIBUTION , ICAS 2006-10.5.3

3. Materials and Structures

MEASUREMENT OF RESIDUAL STRESSES IN ALUMINIUM ALLOY AEROSPACE COMPONENTS , ICAS 2006-P3.5

3. Materials and Structures

MEASURES AND TEST TECHNIQUES OF FUNGUS RESISTANCE TO AIRCRAFT MATERIALS AND EQUIPMENT , ICAS 2006-P3.1

3. Materials and Structures

MICRO-MECHANICAL MODEL OF A SINGLE CRYSTAL NICKEL-BASE SUPERALLOY , ICAS 2006-4.9.1

3. Materials and Structures

MICROWAVE TECHNOLOGIES FOR COMPOSITE PROCESSING , ICAS 2006-4.4.3

3. Materials and Structures

MULTI-DIMENSION LAPLACE WAVELET AND THE APPLICATIONS IN FLIGHT FLUTTER TEST , ICAS 2006-P3.6

3. Materials and Structures

MULTIDISCIPLINARY OPTIMISATION OF CFRP FUSELAGES: STRUCTURAL MECHANICS, VIBRO-ACOUSTICS AND MANUFACTURING ASPECTS , ICAS2006-4.10S

3. Materials and Structures

NANOTECHNOLOGY FOR NOVEL HIGH-PERFORMANCE COMPOSITES: MANUFACTURING, CHARACTERIZATION AND APPLICATION , ICAS 2006-P3.15

3. Materials and Structures

NON LINEAR AEROELASTIC BEHAVIOR OF HIGHLY FLEXIBLE HALE WINGS , ICAS 2006-10.2.4

3. Materials and Structures

NUMERICAL SIMULATION OF C-141 LOWER WING PANELS WITH AND WITHOUT SIMULATED EXFOLIATION CORROSION UNDER COMPRESSION , ICAS 2006-4.9.4

3. Materials and Structures

NUMERICAL SIMULATION OF THE STRUCTURAL BEHAVIOUR OF ORTOTHROPICALLY STIFFENED AIRCRAFT PANELS UNDER SHORT TIME DURATION LOADING , ICAS 2006-10.7.5

3. Materials and Structures

OPTIMISATION OF ENERGY ABSORBING SUBSYSTEM FOR HELICOPTER VERTICAL CRASHES , ICAS 2006-10.7.4

3. Materials and Structures

OPTIMIZATION OF COMPOSITE AIRCRAFT PANELS USING EFFICIENCY ENHANCING EVOLUTIONARY ALGORITHMS , ICAS 2006-4.10.3

3. Materials and Structures

POSTBUCKLING BEHAVIOUR OF A STIFFENED PANEL SUBJECT TO COMBINED LOADING , ICAS 2006-10.4.4

3. Materials and Structures

PROBABILISTIC DESIGN OF ADVANCED COMPOSITE MATERIALS FOR AEROSPACE STRUCTURES , ICAS 2006-4.3.4

3. Materials and Structures

PROCESS INTERACTIONS AND FATIGUE LIFE , ICAS 2006-4.2.1

3. Materials and Structures

PROGRESS ON AIRCRAFT INTEGRATED SAFETY HEALTH ASSESSMENT (AISHA) , ICAS 2006-P3.11

3. Materials and Structures

RELIABILITY ANALYSIS IN  BOLTED COMPOSITE JOINTS WITH SHIMMING MATERIAL , ICAS 2006-4.3.3

3. Materials and Structures

RTM COMPOSITE LUGS FOR HIGH LOAD TRANSFER APPLICATIONS , ICAS 2006-4.4.1

3. Materials and Structures

SIMULATION OF STRUCTURAL BEHAVIOUR OF FIBRE METAL LAMINATE JOINTS , ICAS2006-4.11S

3. Materials and Structures

SMART VORTEX GENERATOR USING SHAPE MEMORY ALLOY , ICAS 2006-4.7.5

3. Materials and Structures

STRESS STAT IN THE  RIVET JOINTS: THE  APPLIED THEORY OF THE FATIGUE FRACTURE , ICAS 2006-4.3.1

3. Materials and Structures

STRUCTURAL BEHAVIOR OF DAMAGED ANISOTROPIC STIFFENED PANELS UNDER COMPRESSIVE LOADS , ICAS2006-4.8S

3. Materials and Structures

STUDY OF FUNDAMENTAL LAMB MODES BEHAVIOUR WITH A SHARP CHANGE OF SECTION IN A PLATE , ICAS 2006-P3.4

3. Materials and Structures

SYNTHESIS AND CHARACTERISATION OF NANO-AL2O3 REINFORCED AA6061 , ICAS 2006-4.9.2

3. Materials and Structures

TAILORED FIBRE PLACEMENT OPTIMIZATION TOOL , ICAS 2006-4.8.3

3. Materials and Structures

TESTING AND MODELING OF FAILURE BEHAVIOR ON FIBER METAL LAMINATES , ICAS 2006-4.1.1

3. Materials and Structures

THE DYNAMIC RESPONSE OF LAMINATE COMPOSITE PLATE UNDER LOW-VELOCITY IMPACT , ICAS 2006-P3.14

3. Materials and Structures

THE EU-FUNDED “ ULTMAT ” PROJECT: ULTRA HIGH TEMPERATURE MATERIALS FOR TURBINES , ICAS 2006-P3.17

3. Materials and Structures

THE MANUFACTURING TECHNOLOGY OF AN ULTRA-PRECISION AEROSTATIC SPINDLE SYSTEM , ICAS 2006-P3.10

3. Materials and Structures

THE ROLE OF OPTIMIZATION IN COMPONENT STRUCTURAL DESIGN: APPLICATION TO THE F-35 JOINT STRIKE FIGHTER , ICAS 2006-4.10.1

3. Materials and Structures

THE SAILPLANE COCKPIT STRUCTURE DURING EMERGENCY LANDING CONDITION , ICAS 2006-10.5.1

3. Materials and Structures

THERMAL ANALYSIS OF HYBRID COMPOSITE STRUCTURES , ICAS 2006-4.6.1

3. Materials and Structures

THROUGH THICKNESS MICROSTRUCTURAL GRADIENTS IN 7475 AND 2022 AGEFORMED BEND COUPONS FOR FUSELAGE AND LOWER WING SKIN APPLICATIONS, ICAS 2006-P3.16

3. Materials and Structures

TOWARDS A METHODOLOGY FOR THE DESIGN OF BIRD-PROOF INTAKES MADE WITH COMPOSITE MATERIAL , ICAS 2006-10.7.2

3. Materials and Structures

VALIDATION PROCEDURE FOR NONLINEAR ANALYSIS OF STRINGER STIFFENED CFRP PANELS , ICAS 2006-10.4.2

3. Materials and Structures

3D FULL PREDICTIVE THERMAL CHAIN FOR GAS TURBINE COMBUSTOR METAL TEMPERATURE , ICAS 2006-5.5.1

4. Propulsion

A TEST RIG FOR INVESTIGATIONS OF GAS TURBINE COMBUSTOR COOLING CONCEPTS UNDER REALISTIC OPERATING CONDITIONS , ICAS 2006-5.3.3

4. Propulsion

AEROELASTIC SIMULATION OF S-DUCT DYNAMICS USING STRUCTURE-COUPLED CFD , ICAS 2006-5.1.3

4. Propulsion

AERO-ENGINE TECHNOLOGY TO COPE WITH ACARE GOALS , ICAS 2006-5.4.5

4. Propulsion

ALTERNATE FUELS AND THEIR POTENTIAL IMPACT TO AVIATION , ICAS 2006-5.8.2 (ISABE):

4. Propulsion

ANALYSIS OF INCREASED COMPRESSION FACTOR ON EJECTOR-ROCKET PERFORMANCE , ICAS 2006-5.2.2

4. Propulsion

APPLICATIONS OF GAME THEORY IN A SYSTEMS DESIGN APPROACH TO STRATEGIC ENGINE SELECTION , ICAS 2006-5.4.1

4. Propulsion

CHALLENGES IN THE HARDWARE IN THE LOOP SIMULATION FOR AN AERO GAS TURBINE ENGINE CONTROL SYSTEM, ICAS 2006-5.4.2

4. Propulsion

CLEAN-  Validation of a GTF High Speed Turbine and Integration of Heat Exchanger Technology in an Environmental Friendly Engine Concept, ICAS 2006-8.10.3

4. Propulsion

COMPRESSOR STABILITY MANAGEMENT IN AIRCRAFT ENGINES  , ICAS2006-5.6S

4. Propulsion

COMPUTATION OF FLOW AND HEAT TRANSFER IN A PRESWIRL ROTOR-STATOR SYSTEM, ICAS2006-5.1S

4. Propulsion

CONTROL OF SUPERSONIC INLET WITH VARIABLE RAMP , ICAS 2006-5.2.4

4. Propulsion

DERIVATION OF AERODYNAMIC THRUST CORRECTION FOR AN INDOOR GAS TURBINE ENGINE TEST FACILITY USING THE "FIRST PRINCIPLES" ANEMOMETER METHOD , ICAS 2006-5.6.4

4. Propulsion

DEVELOPMENT OF A COMBUSTION CHAMBER DESIGN METHODOLOGY AND AUTOMATION OF THE DESIGN PROCESS , ICAS2006-5.5S

4. Propulsion

Development of Air Breathing Engine Theory in Russia: Past, Present and Future , ICAS 2006-8.10.2

4. Propulsion

DEVELOPMENTS IN LOW EMISSIONS COMBUSTION TECHNOLOGY FOR AERO ENGINE APPLICATIONS, ICAS 2006-5.5.3

4. Propulsion

Economy, Profitability and Environmental Compatibility: Challenges in Future Civil Air Transportation; Results of the XVII ISABE Panel Discussion, ICAS 2006-8.9.4

4. Propulsion

EFFECTS OF GAS RADIATION IN SCALED COOLING EFFECTIVENESS TESTS OF TURBINE VANES, ICAS 2006-P4.3

4. Propulsion

Engine Technology Prepared in Europe-   Innovation by Successful Partnerships, ICAS 2006-8.9.1

4. Propulsion

INTERMEDIATE TURBINE DUCT DESIGN AND OPTIMIZATION , ICAS 2006-5.1.1

4. Propulsion

INVESTIGATION OF A COMBUSTOR USING A PRESUMED JPDF REACTION MODEL APPLYING RADIATIVE HEAT LOSS BY THE MONTE CARLO METHOD , ICAS 2006-5.3.2

4. Propulsion

LOW EMISSIONS COMBUSTOR TECHNOLOGY DEVELOPMENTS IN THE EUROPEAN PROGRAMMES LOPOCOTEP AND TLC , ICAS 2006-5.5.2

4. Propulsion

MULTIDISCIPLINARY COMPRESSOR BLADING DESIGN PROCESS USING AUTOMATION AND MULTI-OBJECTIVE OPTIMIZATION , ICAS2006-5.6S

4. Propulsion

MULTIPLE NOZZLE COCEPT IN A SINGLE ENGINE , ICAS 2006-P4.1

4. Propulsion

MULTIPLE NOZZLE COCEPT IN A SINGLE ENGINE , ICAS2006-5.5S

4. Propulsion

NUMERICAL COMPUTATIONS FOR DESIGNING A SCRAMJET INTAKE , ICAS 2006-5.2.3

4. Propulsion

OPTIMIZATION LOOP BASED ON A CFD RANS CODE , ICAS 2006-5.3.1

4. Propulsion

OPTIMUM PITCH ANGLE IN ENGINE INSTALLATION OF A CIVIL JET AIRCRAFT, ICAS 2006-5.4.3

4. Propulsion

PARAMETRIC INTERTURBINE DUCT DESIGN AND OPTIMISATION , ICAS 2006-5.1.2

4. Propulsion

POA ENGINE SYSTEM VALIDATION RIG – AIMS AND CHALLENGES, ICAS 2006-5.6.2

4. Propulsion

Propulsion Systems and Technologies for Future Manned and Unmanned Aerial Vehicles, ICAS 2006-8.10.4

4. Propulsion

RECENT ADVANCES IN THE SIMULATION OF GAS TURBINE SECONDARY AIR SYSTEMS , ICAS 2006-5.4.4

4. Propulsion

RESEARCH AND TECHNOLOGY AT SNECMA TO ENSURE SUSTAINED DEVELOPMENT OF AIR TRANSPORTATION , ICAS 2006-8.9.3

4. Propulsion

STAGNATION-POINT REVERSE FLOW COMBUSTOR PERFORMANCE WITH LIQUID FUEL INJECTION , ICAS 2006-5.3.4

4. Propulsion

THE AITEB PROGRAMME: EUROPEAN RESEARCH FOR IMPROVED HIGH PRESSURE TURBINES, ICAS2006-5.4S

4. Propulsion

The Environmental Challenge-   Bringing Technology to Market, ICAS 2006-8.9.2

4. Propulsion

THE FEASIBILITY OF THE SCRAMJET: AN ANALYSIS BASED ON FIRST PRINCIPLES , ICAS 2006-5.2.1

4. Propulsion

THE INFLUENCE OF FLAME HOLDER GEOMETRY ON THE THRUST INSTABILITY IN A LABORATORIAL SCALE RAMJET ENGINE, ICAS 2006-P4.2

4. Propulsion

TWO SPOOL MORE ELECTRICAL ENGINE, ICAS 2006-5.6.3

4. Propulsion

Validation Methodology for the Development of Low Emission Fuel Injectors for Aero Engines , ICAS 2006-8.10.5

4. Propulsion

VALIDATION OF PROPULSION TECHNOLOGIES AND NEW ENGINE CONCEPTS IN A JOINT TECHNOLOGY DEMONSTRATOR PROGRAM , ICAS 2006-8.10.1

4. Propulsion

VITAL, AN EUROPEAN R&D PROGRAM FOR GREENER AERO-ENGINES , ICAS 2006-5.6.1

4. Propulsion

A NEW APPROACH TO NONLINEAR MODELING OF HIGHLY MANEUVERABLE AIRCRAFT USING NEURAL NETWORKS , ICAS 2006-6.5.3

5. Flight Dynamics and Control

A NEW ARCHITECTURE TO HARMONIZE AUTOMATION WITH PILOT MANEUVER , ICAS 2006-6.9.2

5. Flight Dynamics and Control

ACTUATOR INFLUENCE ON FLYING QUALITIES OF A NATURALLY UNSTABLE AIRCRAFT , ICAS 2006-6.9.4

5. Flight Dynamics and Control

ADAPTIVE NODE DISTRIBUTION FOR ON-LINE TRAJECTORY PLANNING , ICAS 2006-6.3.2

5. Flight Dynamics and Control

AIRCRAFT HEADING CONTROL IN CASE OF INCOMPLETE MEASUREMENT INFORMATION FOR FLY-BY-WIRE CONTROL SYSTEM, ICAS 2006-P5.6

5. Flight Dynamics and Control

AUTONOMOUS TAKE OFF AND LANDING OF THE SHARC TECHNOLOGY DEMONSTRATOR , ICAS 2006-6.7.2

5. Flight Dynamics and Control

BELL M427 FLIGHT TEST DATA GATHERING AND LEVEL-D SIMULATOR MODEL DEVELOPMENT , ICAS 2006-6.10.1

5. Flight Dynamics and Control

CONCEPTION OF AN UAV GENERIC MISSION SYSTEM , ICAS 2006-6.8.1

5. Flight Dynamics and Control

CONTROL SYSTEM DESIGN FOR AN AUTONOMOUS HELICOPTER USING PARTICLE SWARM OPTIMIZATION , ICAS 2006-6.7.4

5. Flight Dynamics and Control

CURVED AND STEEP APPROACH FLIGHT TESTS OF A LOW-COST 3D-DISPLAY FOR GENERAL AVIATION AIRCRAFT , ICAS 2006-6.2.2 INVITED:

5. Flight Dynamics and Control

DESIGN OF A TRACKING CONTROL SYSTEM FOR AN OPTIMAL POST-STALL MANOEUVRE USING DYNAMIC INVERSION APPROACH , ICAS 2006-6.7.3

5. Flight Dynamics and Control

DEVELOPMENT OF A LOW COST FLIGHT DYNAMIC TEST CAPABILITY FOR UAV, ICAS2006-6.8S

5. Flight Dynamics and Control

DEVELOPMENT OF CONTROL LAWS FOR THE SIMULATION OF A NEW TRANSPORT AIRCRAFT , ICAS 2006-6.2.3

5. Flight Dynamics and Control

DEVELOPMENT OF LIGHT AIRCRAFT FLIGHT TEST EQUIPMENT , ICAS2006-6.2S

5. Flight Dynamics and Control

DEVELOPMENT OF THE CONTROL BASED ON THE BIOLOGICAL PRINCIPLES, ICAS 2006-6.4.3

5. Flight Dynamics and Control

FAULT IMMUNE FLIGHT CONTROL SYSTEM FOR CIVIL TRANSPORTS , ICAS 2006-6.4.2

5. Flight Dynamics and Control

FLIGHT CONTROL WITH MINIATURE TRAILING EDGE EFFECTORS , ICAS 2006-6.4.1

5. Flight Dynamics and Control

FLIGHT DYNAMIC SIMULATION OF A FLAPLESS FLIGHT CONTROL UAV , ICAS 2006-6.8.2

5. Flight Dynamics and Control

FLIGHT PLAN AND FLIGHT TEST RESULTS OF EXPERIMENTAL SST VEHICLE NEXST-1 , ICAS 2006-6.2.1 INVITED:

5. Flight Dynamics and Control

FLIGHT SIMULATION FOR THE  PC-21 PROJECT , ICAS 2006-6.10.5

5. Flight Dynamics and Control

FORMATION FLIGHT DESIGN ASPECTS, ICAS 2006-6.6.1 INVITED:

5. Flight Dynamics and Control

FULL ENVELOPE MISSILE AUTOPILOT DESIGN, ICAS2006-6.1S

5. Flight Dynamics and Control

GENERALIZED MISSILE GUIDANCE LAWS AGAINST MANEUVERING TARGETS , ICAS 2006-6.1.3

5. Flight Dynamics and Control

HELICOPTER LOW LEVEL FLIGHT USING TRAJECTORY PLANNING AND OBSTACLE AVOIDANCE , ICAS 2006-6.3.1

5. Flight Dynamics and Control

INTELLIGENT BASED TRAJECTORY PLANNING IN TERRAIN FOLLOWING FLIGHT , ICAS 2006-6.3.3

5. Flight Dynamics and Control

METHOD AND INTEGRATED TOOLS FOR EFFICIENT DESIGN OF AIRCRAFT CONTROL SYSTEMS , ICAS 2006-6.7.5

5. Flight Dynamics and Control

METHOD FOR CALCULATING OBSERVABILITY OF AIRCRAFT FLIGHT ROUTE , ICAS 2006-6.3.4

5. Flight Dynamics and Control

MINC: A MINIATURE INTEGRATED GUIDANCE, NAVIGATION & CONTROL SYSTEM ENABLES IN-FLIGHT GPS/INS DATA FUSION  ABOARD A MICRO AERIAL VEHICLE , ICAS 2006-6.11.1

5. Flight Dynamics and Control

MODEL REDUCTION FOR GPS/SINS INTEGRATED NAVIGATION SYSTEM USING KRYLOV SUBSPACE METHODS , ICAS 2006-6.11.2

5. Flight Dynamics and Control

MULTI-AGENT FORMATION CONTROL FOR UAV SWARMING , ICAS 2006-6.6.2

5. Flight Dynamics and Control

MULTI-BODY MODEL OF FLYING WINGS WITH SIGNIFICANT DEFORMATION , ICAS 2006-6.5.2

5. Flight Dynamics and Control

NEURO-FUZZY CONTROL SYNTHESIS FOR ELECTROHYDRAULIC SERVOS ACTUATING PRIMARY FLIGHT CONTROLS , ICAS 2006-6.4.4

5. Flight Dynamics and Control

NEW PRINCIPLE FOR MISSILE GUIDANCE AND CONTROL , ICAS 2006-6.1.1 INVITED:

5. Flight Dynamics and Control

NONLINEAR MODELING AND SIMULATION OF SMALL-SIZE HELICOPTER DYNAMICS AND MODEL VALIDATION, ICAS 2006-P5.7

5. Flight Dynamics and Control

ON FLIGHT DYNAMICS MODEL IDENTIFICATION AND OPTIMAL FLIGHT TEST PROTOCOL DESIGN , ICAS 2006-6.10.3

5. Flight Dynamics and Control

ON THE EFFECT OF DAMPING AND CONTROLS ON AN AIRCRAFT WAKE ENCOUNTER , ICAS 2006-P5.3

5. Flight Dynamics and Control

OPTIMUM FLIGHT TRAJECTORIES AND SENSITIVITY ANALYSIS FOR TERRAIN COLLISION AVOIDANCE SYSTEMS , ICAS2006-6.3S

5. Flight Dynamics and Control

PARAMETRIC ESTIMATION FLIGHT TEST MANEUVER OPTIMIZATION CONSIDERING MEASUREMENT COLORED RESIDUALS , ICAS 2006-6.10.4

5. Flight Dynamics and Control

POSSIBILITIES AND METHODS OF IN FLIGHT LOADING MEASUREMENTS, ICAS2006-6.2S

5. Flight Dynamics and Control

PRECISION POINTING OF A PAYLOAD SUSPENDED FROM A HIGH ALTITUDE BALLOON, ICAS 2006-6.8.3

5. Flight Dynamics and Control

PREDICTIVE FUNCTIONAL CONTROL AND ITS APPLICATION TO MISSILE CONTROL SYSTEM , ICAS 2006-6.1.2

5. Flight Dynamics and Control

PROGRESS IN PILOT–IN–THE LOOP INVESTIGATIONS FOR FLYING QUALITIES PREDICTION AND EVALUATION , ICAS 2006-6.9.1

5. Flight Dynamics and Control

PROPELLER INSTALLATION EFFECTS ON MULTI-ENGINE PROPELLER AIRCRAFT DIRECTIONAL STABILITY AND CONTROL , ICAS 2006-6.10.2

5. Flight Dynamics and Control

REAL TIME PREDICTION OF SHIP MOTION FOR THE AID OF HELICOPTER AND AIRCRAFT DEPLOYMENT AND RECOVERY , ICAS 2006-P5.4

5. Flight Dynamics and Control

ROBUST CONTROLLERS DESIGN STRATEGIES FOR UNMANNED AIR VEHICLES , ICAS 2006-P5.5

5. Flight Dynamics and Control

ROBUST FLIGHT CONTROL SYSTEM DESIGN WITH GUARANTEED H-INFINITY TYPE PERFORMANCE, ICAS2006-6.7S

5. Flight Dynamics and Control

SEVERAL NEW APPROACHES FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM , ICAS 2006-6.7.1 INVITED:

5. Flight Dynamics and Control

STABILITY AND FLYING QUALITIES ASSESSMENTS OF A SMALL WING-IN-SURFACE-EFFECT TRANSPORT VEHICLE , ICAS 2006-6.5.1

5. Flight Dynamics and Control

STATISTICAL FAULT DETECTION AND IDENTIFICATION IN AIRCRAFT SYSTEMS VIA FUNCTIONALLY POOLED NONLINEAR MODELLING OF FLIGHT DATA DEPENDENCIES , ICAS 2006-6.2.4

5. Flight Dynamics and Control

THE A380 FLIGHT CONTROL SYSTEM : NEW BREAK THROUGH FOR NEW CHALLENGES, ICAS 2006-6.4.5

5. Flight Dynamics and Control

THE APPLICATION OF GAUSSIAN COMPLEX WAVELET IN PIO DETECTION , ICAS 2006-6.9.3

5. Flight Dynamics and Control

THE INFLUENCE OF FREE-  PLAY AND FRICTION IN ELEVATOR CONTROL SYSTEM ON LONGITUDAL DYNAMICS OF THE STRIKE AIRCRAFT , ICAS 2006-P5.2

5. Flight Dynamics and Control

THE STUDY OF INTEGRATED FIRE/FLIGHT/PROPULSION CONTROL (IFFPC) SYSTEM AND DESIGN OF DIGITAL SIMULATION/DESIGN PLATFORM , ICAS 2006-P5.1

5. Flight Dynamics and Control

THROUGH OPTIMIZATION OF BRANCHED TRAJECTORIES WITH RANDOM DISTURBANCES BY THE PONTRYAGIN MAXIMUM PRINCIPLE , ICAS 2006-6.6.3

5. Flight Dynamics and Control

Title: TBD, ICAS 2006-10.8.1 INVITED:

5. Flight Dynamics and Control

Title: TBD, ICAS 2006-10.8.2 INVITED:

5. Flight Dynamics and Control

Title: TBD, ICAS 2006-10.8.3 INVITED:

5. Flight Dynamics and Control

3 AIRCRAFT JOINT TEST TECHNIQUES FOR AIR-TO-AIR SEMI-ACTIVE RADAR-GUIDED MISSILE RADIO FREQUENCY INTERFACE , ICAS 2006-P6.3

6. Systems, Subsystems and Equipments

A COMPARISON OF SOLID OXIDE FUEL CELL DESIGNS AS ENERGY SOURCE FOR THE ALL-ELECTRIC AIRCRAFT , ICAS 2006-7.7.2

6. Systems, Subsystems and Equipments

A NEW HIGH POWER DENSITY GENERATION SYSTEM , ICAS 2006-7.1.1

6. Systems, Subsystems and Equipments

ADAPTIVE LANDING GEARS, ICAS 2006-7.11.3

6. Systems, Subsystems and Equipments

ADVANCED OIL SYSTEM FOR THE ANTLE/POA DEMONSTRATION PLATFORMS , ICAS 2006-7.4.5

6. Systems, Subsystems and Equipments

ADVANCED VERIFICATION AND TEST METHODS FOR DISTRIBUTED CONTROL ARCHITECTURES IN WATER/WASTE SYSTEMS , ICAS 2006-7.6.4

6. Systems, Subsystems and Equipments

AIRCRAFT FUEL SYSTEM DIAGNOSTIC FAULT DETECTION THROUGH EXPERT SYSTEM , ICAS 2006-P6.2

6. Systems, Subsystems and Equipments

AN ELECTRIC COOLING SYSTEM FOR AN UAV , ICAS 2006-7.7.3

6. Systems, Subsystems and Equipments

AN ELECTRICAL FUEL PUMPING AND METERING SYSTEM FOR MORE ELECTRICAL AERO-ENGINES , ICAS 2006-7.4.4

6. Systems, Subsystems and Equipments

AN INNOVATIVE CABIN RECIRCULATION FAN DEMONSTRATOR, ICAS 2006-P6.5

6. Systems, Subsystems and Equipments

AN INNOVATIVE TOOL FOR AIRCRAFT EQUIPMENT SYSTEMS INTEGRATION AND ELECTRICAL NETWORK CHARACTERISATION, ICAS2006-7.2S

6. Systems, Subsystems and Equipments

AN INTEGRATED MACHINE AND MATRIX CONVERTER BASED HIGH POWER RUDDER EMA , ICAS 2006-7.4.3

6. Systems, Subsystems and Equipments

ANALYSIS OF A FEASIBLE PULSED-POWER SUPPLY SYSTEM FOR AN UNMANNED AERIAL VEHICLE , ICAS 2006-7.1.3

6. Systems, Subsystems and Equipments

ANALYSIS OF AIRCRAFT COMPRESSOR SYSTEMS , ICAS 2006-7.7.5

6. Systems, Subsystems and Equipments

AVIONIC OPTICAL LINKS FOR HIGH DATA-RATE COMMUNICATIONS , ICAS 2006-7.9.1

6. Systems, Subsystems and Equipments

CLOSED-LOOP SIMULATION WITH FLIGHT CONTROL ACTUATORS, ICAS 2006-7.10.5

6. Systems, Subsystems and Equipments

COMPARISON OF POWER QUALITY SOLUTIONS USING ACTIVE AND PASSIVE RECTIFICATION FOR MORE ELECTRIC AIRCRAFT , ICAS 2006-7.5.2

6. Systems, Subsystems and Equipments

CONSIDERATION OF FUEL CONSUMPTION CAUSED BY AIRCRAFT SYSTEMS IN AIRCRAFT DESIGN , ICAS 2006-7.2.4

6. Systems, Subsystems and Equipments

CONTINUOUS SIMULATION SUPPORT DURING THE DEVELOPMENT PROCESS OF A FUEL CELL SYSTEM ON BOARD OF CONVENTIONAL AIRCRAFT , ICAS 2006-7.3.2

6. Systems, Subsystems and Equipments

CONTROLLABLE STUDY OF ELECTRO-RHEOLOGICAL FLUID APPLIED TO LANDING GEAR BUMPER , ICAS 2006-7.11.1

6. Systems, Subsystems and Equipments

ELECTRICAL ROTATING MACHINES AND POWER ELECTRONICS FOR NEW AIRCRAFT EQUIPMENT SYSTEMS , ICAS 2006-7.1.2

6. Systems, Subsystems and Equipments

ELECTRICALLY POWERED ICE PROTECTION SYSTEMS FOR MALE UAVS – REQUIREMENTS AND INTEGRATION CHALLENGES , ICAS 2006-7.3.3

6. Systems, Subsystems and Equipments

ELECTRIFICATION OF THE ENVIRONMENTAL CONTROL SYSTEM , ICAS 2006-7.7.1

6. Systems, Subsystems and Equipments

ENVIRONMENTAL CHALLENGE TO AIRBORNE ELECTRONIC EQUIPMENT MAINTENANCE , ICAS 2006-P6.1

6. Systems, Subsystems and Equipments

FAULT-  TOLERANT PROCEDURES FOR AIR DATA ELABORATION , ICAS 2006-7.9.4

6. Systems, Subsystems and Equipments

FORMULATION AND IMPLEMENTATION OF AN AIRCRAFT – SYSTEM – SUBSYSTEM INTERRELATIONSHIP MODEL FOR TECHNOLOGY EVALUATION , ICAS 2006-7.10.2

6. Systems, Subsystems and Equipments

FUEL CELL SYSTEMS FOR AERONAUTIC APPLICATIONS: A CLEAN WAY FROM KEROSENE TO ENERGY , ICAS 2006-7.3.1

6. Systems, Subsystems and Equipments

GENERATOR POWER OPTIMISATION FOR A MORE-ELECTRIC AIRCRAFT BY USE OF A VIRTUAL IRON BIRD , ICAS 2006-7.5.1

6. Systems, Subsystems and Equipments

HIGH POWER PIEZOELECTRIC MOTOR FOR BRAKE ACTUATOR-  PIBRAC PROJECT , ICAS 2006-7.3.4

6. Systems, Subsystems and Equipments

HIGH SPEED OPTICAL FIBER TRANSMISSION TECHNOLOGY FOR AVIONICS APPLICATIONS , ICAS2006-7.9S

6. Systems, Subsystems and Equipments

INITIAL TEST RESULTS FOR THE FAN SHAFT DRIVEN GENERATOR , ICAS2006-7.1S

6. Systems, Subsystems and Equipments

LABINAL CURRENT WORK TOWARDS THE MORE ELECTRICAL AIRCRAFT THROUGH THE POA EUROPEAN PROGRAMME, ICAS2006-7.5S

6. Systems, Subsystems and Equipments

LATEST DEVELOPMENTS IN LANDING GEARS, ICAS 2006-7.8.1 INVITED:

6. Systems, Subsystems and Equipments

METHODS FOR THE DESIGN OF ENERGY EFFICIENT HIGH-SPEED AEROSPACE VEHICLES , ICAS 2006-7.10.1

6. Systems, Subsystems and Equipments

MIXED CONVECTION IN A FULL SCALE AIRCRAFT CABIN MOCK-UP , ICAS 2006-7.6.3

6. Systems, Subsystems and Equipments

MODEL-BASED DIAGNOSIS STUDIES OF COMPLEX FLUID MECHANICAL AIRCRAFT SYSTEMS , ICAS2006-7.10S

6. Systems, Subsystems and Equipments

ON-BOARD WIND MEASUREMENT SYSTEM BASED ON MINIATURIZED NAVIGATION SENSORS , ICAS 2006-7.9.3

6. Systems, Subsystems and Equipments

OPTIMIZATION OF A SPUR GEAR PROFILE FOR MINIMUM TRANSMISSION ERROR OF A GEAR SET USING GENETIC ALGORITHM, ICAS2006-7.10S

6. Systems, Subsystems and Equipments

PASSENGER ACCEPTABILITY ASSESSMENT MODEL-METHODOLOGY FOR FUTURE CUSTOMER-ORIENTATED AIRCRAFT CABIN DESIGN , ICAS 2006-7.6.1

6. Systems, Subsystems and Equipments

POWER BY WIRE, AN OPPORTUNITY?, ICAS 2006-7.2.2

6. Systems, Subsystems and Equipments

REAL-TIME HARDWARE-IN-THE-LOOP SIMULATION OF FLY-BY-WIRE FLIGHT CONTROL SYSTEMS , ICAS 2006-7.10.4

6. Systems, Subsystems and Equipments

SIMULATION AND ANALYSIS OF A NEW HIGH POWER DENSITY GENERATOR , ICAS2006-7.5S

6. Systems, Subsystems and Equipments

SIMULATION OF FLUID MECHANICAL AIRCRAFT SYSTEMS FROM CONCEPT EVALUATION TO QUALIFICATION TESTS , ICAS 2006-7.10.3

6. Systems, Subsystems and Equipments

SIMULATION OF LANDING GEAR DYNAMICS USING FLEXIBLE MULTI-BODY METHODS , ICAS 2006-7.8.3

6. Systems, Subsystems and Equipments

SIMULATION WITH MODELICA FOR A DYNAMIC REPRESENTATION OF AN AIRCRAFT CABIN CLIMATE FOR COMFORT-IMPROVED CLIMATE CONTROL , ICAS 2006-7.6.2

6. Systems, Subsystems and Equipments

SMALL-SIGNAL STABILITY STUDIES OF 270V DC POWER SYSTEM FOR MORE ELECTRIC AIRCRAFT EMPLOYING SWITCHED RELUCTANCE GENERATOR TECHNOLOGY , ICAS 2006-7.5.3

6. Systems, Subsystems and Equipments

SUBSYSTEM DESIGN AND INTEGRATION FOR THE MORE ELECTRIC AIRCRAFT , ICAS 2006-7.2.3 INVITED:

6. Systems, Subsystems and Equipments

SUMMARY OF THE EUROPEAN POWER OPTIMISED AIRCRAFT (POA) PROJECT , ICAS 2006-7.2.1

6. Systems, Subsystems and Equipments

THE A380 FLIGHT CONTROL ELECTROHYDROSTATIC ACTUATORS, ACHIEVEMENTS AND LESSONS LEARNT , ICAS 2006-7.4.1

6. Systems, Subsystems and Equipments

THE DESIGN OF A SERIES OF ELECTROTHERMAL ICE PROTECTION SYSTEMS , ICAS 2006-P6.4

6. Systems, Subsystems and Equipments

THE DEVELOPMENT OF A ROBUST AIRCRAFT ANTI-SKID CONTROLLER UTILISING MU-SLIP GRADIENT CONTROL, ICAS 2006-7.11.2

6. Systems, Subsystems and Equipments

THE NEED FOR A MORE EFFICIENT ALTERNATIVE TO THE ENGINE BLEED AIR OPERATED WING ICE PROTECTION SYSTEM, ICAS2006-7.7S

6. Systems, Subsystems and Equipments

THE USE OF A HYBRID ACTUATION PACKAGE FOR IMPROVED EFFICIENCY IN ELECTRICALLY POWERED FLIGHT ACTUATION, ICAS 2006-7.4.2

6. Systems, Subsystems and Equipments

TOWARD A FIPA COMPLIANT MULTI-AGENT REAL-TIME ARCHITECTURE FOR INTEGRATED MODULAR AVIONICS , ICAS 2006-7.9.2

6. Systems, Subsystems and Equipments

TRANSIENT SIMULATION OF A DIRECT-EVAPORATING CO2 COOLING SYSTEM FOR AN AIRCRAFT , ICAS 2006-7.7.4

6. Systems, Subsystems and Equipments

ULTIMATE POWER OPTIMIZING FOR A ‘STAND ALONE’ LANDING GEAR SYSTEM OF MORE ELECTRIC AIRCRAFT (MEA) , ICAS 2006-7.8.2

6. Systems, Subsystems and Equipments

A 3D KNOWLEDGE-BASED ROUTER FOR WIRING IN AEROSPACE VEHICLES , ICAS 2006-9.3.4

7. Systems Engineering an Supply Chain

AGEFORMABLE PANELS FOR COMMERCIAL AIRCRAFT , ICAS 2006-9.1.3

7. Systems Engineering an Supply Chain

AN ALGORITHMIC MORPHOLOGY MATRIX FOR AIRCRAFT FUEL SYSTEM CONCEPTUAL DESIGN , ICAS 2006-9.2.2

7. Systems Engineering an Supply Chain

COMPUTATIONAL DESIGN PROCESS MODELLING , ICAS 2006-9.2.3

7. Systems Engineering an Supply Chain

EVIDENCE OF LEAN ENGINEERING IN AIRCRAFT PROGRAMS , ICAS 2006-9.4.1

7. Systems Engineering an Supply Chain

FINDING THE REAL VALUE OF ADAPTABLE  VEHICLE CONFIGURATIONS IN AN UNCERTAIN WORLD , ICAS 2006-9.4.4

7. Systems Engineering an Supply Chain

INFUSION TECHNOLOGY FOR AUTOMATED PRODUCTION OF HIGH PERFORMANCE  CFRP-PARTS , ICAS 2006-9.1.2

7. Systems Engineering an Supply Chain

KNOWLEDGE ENABLED PROCESS ENGINEERING-  REVOLUTION OR ADAPTATION , ICAS 2006-9.3.1

7. Systems Engineering an Supply Chain

MANUFACTURING CHALLENGES AND EXPERIENCES FROM A380, ICAS 2006-9.1.1 INVITED:

7. Systems Engineering an Supply Chain

METHODOLOGY FOR THE DESIGN AND EVALUATION OF WING LEADING EDGE AND TRAILING EDGE DEVICES , ICAS 2006-9.2.1

7. Systems Engineering an Supply Chain

METHODS FOR ENGINEERING CHANGE PROPAGATION ANALYSIS , ICAS 2006-9.3.3

7. Systems Engineering an Supply Chain

RELATIVE LIFE-CYCLE-COST ESTIMATION OF FUTURE SPACE TRANSPORTATION SYSTEMS AT CONCEPTUAL DESIGN PHASE , ICAS 2006-9.4.3

7. Systems Engineering an Supply Chain

SCENARIO-BASED DESIGN COMPETITIVENESS EXPLORATION WITH SYSTEM DYNAMICS , ICAS 2006-9.4.2

7. Systems Engineering an Supply Chain

THE RESEARCH ON AIRCRAFT RDT&E COST BASED ON GRAY CORRELATION ANALYSIS THEORY AND EQUALATION-ENGINEERING-VALUE-RATE , ICAS 2006-9.4.5

7. Systems Engineering an Supply Chain

TOP DOWN CAD MODELING METHODOLOGY FOR LOW PRESSURE TURBINE DESIGN , ICAS2006-9.2S

7. Systems Engineering an Supply Chain

TOWARDS ROBUST ORDER PROCESSING THROUGH QUALITY INTELLIGENCE , ICAS 2006-9.3.2

7. Systems Engineering an Supply Chain

TRANSFER OF ADVANCED ASAAC SW TECHNOLOGY ONTO THE EUROFIGHTER/TYPHOON , ICAS 2006-9.2.4

7. Systems Engineering an Supply Chain

USING VIRTUAL ASSEMBLY TECHNOLOGY TO DESIGN AND DEVELOP THE ARJ21 BUSINESS JET BASE ON CATIA V5 AND ENOVIA VPM , ICAS 2006-P7.1

7. Systems Engineering an Supply Chain

"FILE AND FLY"-  PROCEDURES AND TECHNIQUES FOR INTEGRATION OF UAVS IN CONTROLLED AIRSPACE , ICAS 2006-8.4.1

8. Air Transport System Efficiency

4D TRAJECTORY MANAGEMENT IN THE EXTENDED TMA: COUPLING AMAN AND 4D FMS FOR OPTIMIZED APPROACH TRAJECTORIES , ICAS 2006-8.8.2

8. Air Transport System Efficiency

A DECISION SUPPORT SYSTEM FOR HELICOPTER EMERGENCY MEDICAL SERVICE OPERATIONS , ICAS 2006-8.3.2

8. Air Transport System Efficiency

AIRCRAFT PARAMETER AND PROCEDURE DRIVEN SIMULATION OF AIRPORT AIRSIDE OPERATIONS , ICAS 2006-8.8.1

8. Air Transport System Efficiency

AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION PACKAGE-  WAKESCENE , ICAS 2006-8.6.3

8. Air Transport System Efficiency

AN AGENT-BASED MODEL FOR ANALYZING CONTROL POLICIES AND THE DYNAMIC SERVICE-TIME PERFORMANCE OF A CAPACITY-CONSTRAINED AIR TRAFFIC MANAGEMENT FACILITY , ICAS 2006-8.4.2

8. Air Transport System Efficiency

AUTOMATED CONFLCIT RESOLUTION FOR AIR TRAFFIC CONTROL , ICAS 2006-8.2.1

8. Air Transport System Efficiency

CHANGES IN AIRPORT TERMINAL DESIGN, ICAS 2006-P8.3

8. Air Transport System Efficiency

CONTRIBUTION TO THE OPERATIONAL EVALUATION OF EGNOS AS AN AERONAUTICAL NAVIGATION SYSTEM , ICAS 2006-8.2.3

8. Air Transport System Efficiency

DEVELOPMENT PROBLEMS OF THE VILNIUS AND KAUNAS AIRPORTS , ICAS2006-8.5S

8. Air Transport System Efficiency

EFFICIENCY DRIVEN BY JOINT OBJECTIVES: A NEW WAY TO ORGANIZE THE AIR TRAFFIC MANAGEMENT , ICAS 2006-8.2.2

8. Air Transport System Efficiency

EMMA-  EUROPEAN AIRPORT MOVEMENT MANAGEMENT BY A-SMGCS-  A CONTRIBUTION TO THE VISION 2020 , ICAS 2006-8.5.3

8. Air Transport System Efficiency

ESTIMATION OF DAILY UNSCHEDULED LINE MAINTENANCE EVENTS IN CIVIL AVIATION , ICAS2006-8.3S

8. Air Transport System Efficiency

FUTURE DEVELOPMENTS IN ATM-  EUROPÉ, ICAS 2006-8.7.1 INVITED:

8. Air Transport System Efficiency

FUTURE DEVELOPMENTS IN ATM-  USA, ICAS 2006-8.7.2 INVITED:

8. Air Transport System Efficiency

FUTURE DEVELOPMENTS IN ATM-  JAPAN , ICAS 2006-8.7.3 INVITED:

8. Air Transport System Efficiency

HUMAN FACTORS CONSIDERATIONS FOR AREA NAVIGATION DEPARTURE AND ARRIVAL PROCEDURES , ICAS 2006-8.2.4

8. Air Transport System Efficiency

IMAGE PROCESSING TECHNOLOGY OF FLIR-BASED ENHANCED VISION SYSTEM , ICAS 2006-P8.2

8. Air Transport System Efficiency

IMPACT OF INDIVIDUAL AND DYNAMIC WAKE VORTEX SEPARATIONS ON AIRPORT CAPACITY , ICAS 2006-8.6.2

8. Air Transport System Efficiency

INCREASING RUNWAY CAPACITY USING GENETIC ALGORITHMS AND ENHANCED HEURISTICS , ICAS 2006-8.5.2

8. Air Transport System Efficiency

INTERMODAL INTEGRATION OF LARGE VOLUME AIR CARGO , ICAS2006-8.5S

8. Air Transport System Efficiency

KNOWLEDGE MANAGEMENT CONCEPTS FOR AIR TRANSPORT SYSTEMS ARCHITECTING , ICAS 2006-8.4.5

8. Air Transport System Efficiency

LASER LIGHT LANDING SYSTEM (LS3) , ICAS 2006-P8.1

8. Air Transport System Efficiency

MODELS AND PROCEDURES FOR THE ASSESSMENT OF FUTURE MAINTENANCE TECHNOLOGIES FOR NEXT-GENERATION AIRLINERS WITHIN THE FUZZY FRONT END OF THE INNOVATION PROCESS , ICAS 2006-8.3.4

8. Air Transport System Efficiency

MONTE CARLO ANALYSIS OF AIRPORT THROUGHPUT AND TRAFFIC DELAYS USING SELF SEPARATION PROCEDURES , ICAS 2006-8.8.3

8. Air Transport System Efficiency

OPERATIONAL FEASIBILITY OF TRAFFIC SYNCHRONISATION IN CENTRAL EUROPE-  RESULTS , ICAS 2006-8.4.3

8. Air Transport System Efficiency

PAVE: ASSISTANCE SYSTEM TO SUPPORT PILOTS FOR IFR ROTORCRAFT AIRPORT OPERATIONS , ICAS 2006-8.3.1

8. Air Transport System Efficiency

PERSPECTIVES OF AIR TRAFFIC MANAGEMENT SYSTEM IN RUSSIA , ICAS 2006-8.7.4 INVITED:

8. Air Transport System Efficiency

POINT-TO-POINT!  VALIDATION OF THE SMALL AIRCRAFT TRANSPORTATION SYSTEM HIGHER VOLUME OPERATIONS CONCEPT , ICAS 2006-8.4.4

8. Air Transport System Efficiency

POTENTIAL FOR TRANSPORT EFFICIENCY IMPROVEMENTS OF AVIATION TRANSPORTATION SYSTEMS , ICAS2006-8.2S

8. Air Transport System Efficiency

PROSPECTS FOR HEAD- AND CROSSWIND DEPENDENT AIRCRAFT SEPARATIONS IN THE CONTEXT OF WAKE VORTEX SAFETY AND AIRPORT CAPACITY, APPLICATION TO SCHIPHOL AIRPORT , ICAS 2006-8.6.1

8. Air Transport System Efficiency

REAL-TIME AIRCRAFT NOISE PREDICTION FOR TRAJECTORY BASED ARRIVAL MANAGERS , ICAS 2006-8.11.1

8. Air Transport System Efficiency

REAL-TIME SIMULATION STUDIES CONCERNING THE OPERATIONAL ASPECTS OF TWO LANDING THRESHOLDS ON ONE RUNWAY AT FRANKFURT/M , ICAS 2006-8.11.2

8. Air Transport System Efficiency

SNOWFLAKE-  DESIGNING AND ORGANISING A WINTER EXERCISE FOR AMSTERDAM AIRPORT SCHIPHOL , ICAS 2006-8.11.3

8. Air Transport System Efficiency

SPADE: SUPPORTING PLATFORM FOR AIRPORT DECISION-MAKING AND EFFICIENCY ANALYSIS , ICAS 2006-8.5.1

8. Air Transport System Efficiency

SUMMARY OF NOCTARN RESEARCH PROJECT , ICAS 2006-8.3.3

8. Air Transport System Efficiency

SYSTEM-OF-SYSTEMS SIMULATION FOR ANALYZING THE EVOLUTION OF AIR TRANSPORTATION , ICAS 2006-8.7.5

8. Air Transport System Efficiency

AIRBUS FLY-BY-WIRE: A PROCESS TOWARD TOTAL DEPENDABILITY , ICAS 2006-9.9.1

9. Safety and Security

AIRCRAFT SECURITY : EVOLUTION OF COCKPIT RESOURCE MANAGEMENT & COCKPIT VIDEO TRANSMISSION, ICAS2006-9.10S

9. Safety and Security

AIRPORT SAFETY MANAGEMENT SYSTEM FOR THE FUTURE , ICAS 2006-10.9.4

9. Safety and Security

AUTOMATIC GUIDANCE FOR TRAFFIC AVOIDANCE-  APFD TCAS MODE, ICAS 2006-9.9.2

9. Safety and Security

CONCEPTS FOR ENERGY ABSORBING SUPPORT STRUCTURES AND APPROPRIATE MATERIALS , ICAS 2006-9.6.4

9. Safety and Security

CONFLICT AND SEPARATION SYMBOLS IN CDTI FOR SMALL AIRCRAFT OPERATION , ICAS 2006-9.10.5

9. Safety and Security

DETERMINATION OF SMOKE QUANTITIES TO BE USED FOR SMOKE DETECTION PERFORMANCE GROUND AND FLIGHT TESTS , ICAS 2006-9.8.2

9. Safety and Security

DEVELOPEMENT OF A PRODUCTION ORGANIZATION EXPOSITION SCHEME TAKING INTO ACCOUNT EN9100 REQUIREMENTS , ICAS 2006-P9.2

9. Safety and Security

DEVELOPMENT OF A METHOD FOR CRM SKILLS MEASUREMENT , ICAS 2006-9.7.4

9. Safety and Security

DEVELOPMENT OF HELICOPTER SAFETY DEVICES , ICAS2006-9.6S

9. Safety and Security

ELECTRONIC SYSTEM FOR DEACTIVATION OF CLOCK-ACTIVATED BOMBS WITH THE HELP OF LIQUID NITROGEN , ICAS 2006-P9.3

9. Safety and Security

ENHANCEMENTS OF FLIGHT MANAGEMENT SYSTEM WITH INTEROPERABILITY , ICAS 2006-P9.5

9. Safety and Security

ENTROPY METHOD OF RELIABILITY ASSESSMENT FOR AIRCRAFT SYSTEMS , ICAS2006-8.1S

9. Safety and Security

EVALUATION ON FLIGHT MANAGEMENT SKILL OF JET AIRLINER PILOTS-  A CASE OF GO-AROUND- , ICAS 2006-9.10.4

9. Safety and Security

EVS BASED APPROACH PROCEDURES: IR IMAGE ANALYSIS AND IMAGE FUSION TO SUPPORT PILOTS IN LOW VISIBILITY , ICAS2006-9.9S

9. Safety and Security

FLEET USAGE MONITORING IS ESSENTIAL IN IMPROVING AGING U.S. ARMY HELICOPTER RELIABILITY AND MAINTAINABILITY , ICAS 2006-8.1.1

9. Safety and Security

FULL-SCALE CRASH TEST OF A CIVIL HELICOPTER AT JAXA , ICAS 2006-9.6.1

9. Safety and Security

HEAD-UP GUIDANCE SYSTEM MODEL 2100 AND HUMAN-MACHINE INTERACTION , ICAS 2006-9.10.1

9. Safety and Security

HELICOPTER SUBFLOOR-INTEGRATED FUEL-TANK CRASHWORTHINESS , ICAS 2006-9.6.3

9. Safety and Security

HYDROGEN TECHNOLOGY – READY FOR TAKE-OFF – HYDROGEN APPLICATIONS IN AEROSPACE INDUSTRY , ICAS 2006-P9.4

9. Safety and Security

IMPACT OF WORKPLACE ENVIRONMENT ON HEALTH AND COMFORT OF FLIGHT ATTENDANTS AND PILOTS- RESULTS FROM THE EU PROJECT HEACE , ICAS 2006-9.7.1

9. Safety and Security

IMPROVED WEATHER INFORMATION FOR COCKPIT AND TOWER , ICAS 2006-9.5.2

9. Safety and Security

INCORPORATING DATA LINK MESSAGING INTO A MULTI-FUNCTION DISPLAY FOR GENERAL AVIATION AIRCRAFT , ICAS 2006-9.9.3

9. Safety and Security

INCREASING AVIATION SAFETY BY ASSESSING ENGLISH LANGUAGE PROFICIENCY AMONG AVIATION POFESSIONALS , ICAS2006-9.7S

9. Safety and Security

INTRODUCTION OF DUAL THRESHOLD OPERATION IN FRANKFURT/MAIN-  EVALUATION OF HUMAN-FACTORS FROM THE PILOT’S PERSPECTIVE, ICAS2006-9.7S

9. Safety and Security

NEW TECHNOLOGIES FOR REDUCING AVIATION WEATHER-RELATED ACCIDENTS , ICAS 2006-9.5.1

9. Safety and Security

ON AN ABSOLUTE SAFETY CRITERION FOR THE PROBABILITY OF THE COLLISION BETWEEN AIRCRAFT , ICAS 2006-9.5.3

9. Safety and Security

ON THE CONNECTION BETWEEN PILOT'S PERFORMANCE AND INCREASING COMPLEXITY OF FLIGHT SIMULATION SYSTEMS , ICAS 2006-9.7.2

9. Safety and Security

ON THE VALIDATION OF HELICOPTER FLIGHT SIMULATORS OPERATING IN EMERGENCY PROCEDURES , ICAS 2006-8.1.3

9. Safety and Security

PEDESTRIAN DYNAMICS IN AIRPORT TERMINALS CONSIDERING EMERGENCY CASES , ICAS 2006-10.9.3

9. Safety and Security

PILOT EVALUATION OF A TAKE-OFF MONITOR DISPLAY , ICAS 2006-9.9.4

9. Safety and Security

PILOT GAZE AND PERFORMANCE WITH RESPECT TO SITUATION AWARENESS, ICAS 2006-9.7.3

9. Safety and Security

PILOTING COGNITIVE PERFORMANCE: THE EUCALEPIC EFFECT IN THE COCKPIT, ICAS 2006-9.7.5

9. Safety and Security

PILOT-IN-THE-LOOP EVALUATION OF NEXT GENERATION WEATHER RADAR DISPLAYS , ICAS 2006-9.10.3

9. Safety and Security

RELIABILITY ASSESSMENT OF COMPLEX ELECTRO-MECHANICAL SYSTEMS TAKING INTO ACCOUNT SYSTEM-STRUCTURE INTERACTION., ICAS 2006-8.1.2

9. Safety and Security

RESEARCH ON RELIABILITY GROWTH TECHNOLOGY OF ELECTROMECHANICAL-HYDRAULIC SYSTEM , ICAS 2006-P9.6

9. Safety and Security

RISK ASSESSMENT OF NEWLY PROPOSED SYSTEMS TO IMPROVE IN-FLIGHT SECURITY , ICAS 2006-10.9.2

9. Safety and Security

SAFEE: SECURITY OF AIRCRAFT IN THE FUTURE EUROPEAN ENVIRONMENT, ICAS 2006-10.9.1

9. Safety and Security

SAFETY FOR LITTLE TRAVELERS-  CHILD RESTRAINT SYSTEMS-  GETTING SAFELY OFF THE GROUND, ICAS2006-9.8S

9. Safety and Security

SELECTION OF PARAMETERS IN FIXED-DURATION RELIABILITY QUALIFICATION TEST SCHEME , ICAS 2006-P9.1

9. Safety and Security

STUDIES ON THE PERFORMANCE OF SMOKE DETECTORS AND THEIR HOUSING IN AN AIRCRAFT CARGO COMPARTMENT ENVIRONMENT , ICAS 2006-9.8.1

9. Safety and Security

THE RESEARCH DEVELOPMENT OF MAN-MACHINE-ENVIRONMENT SYSTEM ENGINEERING TECHNOLOGY IN THE AIRCRAFT DESIGN OF CHINA , ICAS 2006-9.10.2

9. Safety and Security

USING DETECTION INDICES (DIS) TO DETECT AIR VEHICLE CHARACTERISTIC CHANGES FOR HUMS APPLICATION , ICAS 2006-9.8.3

9. Safety and Security

VIRTUAL CO-PILOT SYSTEM IN GENERAL AVIATION, ICAS2006-9.9S

9. Safety and Security

A STRATEGY TOWARDS SUSTAINABLE DEVELOPMENT OF UK AVIATION , ICAS 2006-5.10.1 INVITED:

10. Challenge of the Environment

ADVANCED LINER COOLING NUMERICAL ANALYSIS FOR LOW EMISSION COMBUSTORS , ICAS 2006-5.8.3

10. Challenge of the Environment

AERONET III “AIRCRAFT EMISSIONS AND REDUCTION TECHNOLOGIES”, A EUROPEAN FUNDED COORDINATION ACTION, ICAS 2006-P10.1

10. Challenge of the Environment

AN ALGEBRAIC APPROACH TO AGGREGATE SUBJECT RESPONSE IN AIRCRAFT NOISE MANAGEMENT, ICAS2006-5.10S

10. Challenge of the Environment

AVIATION ENVIRONMENTAL POLICY ASSESSMENT THROUGH DYNAMIC SIMULATION , ICAS 2006-5.10.3

10. Challenge of the Environment

BENCHMARKING AND VALIDATION OF PREDICTION METHODS FOR LOW NOISE AIRCRAFT DESIGN, ICAS 2006-5.7.4

10. Challenge of the Environment

CLIMATE CHANGE IMPACT OF AIR TRAFFIC , ICAS 2006-5.9.1

10. Challenge of the Environment

CONTRAIL AND CIRRUS CLOUD AVOIDANCE , ICAS2006-5.9S

10. Challenge of the Environment

DEVELOPING QUIETER AIRCRAFT, ICAS 2006-5.7.2

10. Challenge of the Environment

DEVELOPMENT OF SILENT AIRFRAME CONCEPTS AND INNOVATIVE CYCLE PROPULSION SYSTEMS FOR REDUCTION IN AIRCRAFT NOISE , ICAS 2006-5.7.3

10. Challenge of the Environment

DO AIRCRAFT BLACK CARBON EMISSIONS AFFECT CIRRUS CLOUDS ON THE GLOBAL SCALE ? , ICAS2006-5.9S

10. Challenge of the Environment

ECATS-  A EUROPEAN NETWORK OF EXCELLENCE FOR AN ENVIRONMENTAL AIR TRANSPORT SYSTEM, ICAS 2006-P10.2

10. Challenge of the Environment

HIGH-RESOLUTION WEATHER FORECAST EXPERIMENTS ON THE EARTH SIMULATOR: CONNECTIONS TO AERONAUTICS , ICAS 2006-5.9.3 INVITED:

10. Challenge of the Environment

HOLISTIC APPROACH FOR ENVIRONMENTALLY FRIENDLY AIRCRAFT DESIGN , ICAS 2006-5.10.5

10. Challenge of the Environment

OPERATIONAL ISSUES ASSOCIATED WITH AN ADAPTIVE CONTRAIL AVOIDANCE POLICY, ICAS 2006-5.9.4

10. Challenge of the Environment

ORGANISATION OF EUROPEAN AERONAUTIC ULTRA-LOW NOX COMBUSTION RESEARCH , ICAS 2006-5.8.1

10. Challenge of the Environment

REDUCING THE ENVIRONMENTAL IMPACT OF AVIATION BY USING SUSTAINABLE DEVELOPMENT INDICATORS , ICAS 2006-5.10.4

10. Challenge of the Environment

SUSTAINING AVIATION GROWTH- MEETING THE ENVIRONMENTAL CHALLENGES , ICAS 2006-5.10.2 INVITED:

10. Challenge of the Environment

THE BOEING QUIET TECHNOLOGY DEMONSTRATOR PROGRAM , ICAS 2006-5.7.1 INVITED:

10. Challenge of the Environment

USING FAA’S SAGE MODEL TO CONDUCT GLOBAL INVENTORIES AND TO ASSESS ROUTE-SPECIFIC VARIABILITY IN AVIATION FUEL BURN, EMISSIONS AND COSTS , ICAS 2006-5.9.2

10. Challenge of the Environment