ICAS 2004: TOPICS AND TITLES


ICAS DANIEL & FLORENCE GUGGENHEIM MEMORIAL LECTURE
VON KARMAN LECTURE

General Lectures


Aerodynamics
Air Transport System Efficiency

Aircraft and Systems Integration
Challenge of the Environment

Flight Dynamics and Control

Materials and Structures
Propulsion
Propulsion/ISABE

Safety and Security
Systems Engineering and Supply Chain
Systems, Subsystems and Equipments


A Complex Method for Numerical Optimization on Airfoil, ICAS 2004-2.7.4 (St.) Aerodynamics
A Drag Prediction Validation Study for Aircraft Aerodynamic Analysis, ICAS 2004-2.3.1 Aerodynamics
A Fast Viscous Correction Method Applied to Small Disturbance Potential Transonic Flows in the Frequency Domain, ICAS 2004-2.1.R.2 Aerodynamics
A General Method for Structured Grid Generation Using, ICAS 2004-2.4.R.2 Aerodynamics
A Mechanism of Sound Generation from Vortex Predominant Flows, ICAS 2004-3.4.1 Aerodynamics
A New Calculation Method of Compressible Flow, ICAS 2004-2.4.2 (St.) Aerodynamics
A Novel Facility for Testing at Low Reynolds Number, ICAS 2004-3.1.3 Aerodynamics
A Numerical Study of Drag and Heat Transfer to Blunt Nose Shapes in Rarefied Hypersonic Flow, ICAS 2004-3.7.2 Aerodynamics
A PIV and CFD Investigation of Cavity Flows in the Transonic Flow Regime, ICAS 2004-4.2.2 Aerodynamics
A Time Accurate Zonal Finite Element Method for Solving Compressible and Incompressible Viscous Flows, ICAS 2004-2.4.4 Aerodynamics
A Viscous-Inviscid Interaction for Aerodynamic and Aeroelastic Calculation, ICAS 2004-2.2.R.1 Aerodynamics
A Wind Tunnel Based Study of the Flow Field behind Sailplane Winglets, ICAS 2004-2.11.1 Aerodynamics
Active Separation Control on a High-Lift Configuration by a Periodically Pulsating Jet, ICAS 2004-3.9.1 Aerodynamics
Active Separation Control with Longitudinal Vortices Generated by Three Types of Jet Orifice Shape, ICAS 2004-3.9.2 Aerodynamics
Advances in CFD-Methods for Vortical and Separated Flows of High Maneuverable Aircraft, ICAS 2004-2.5.1 (I.L.) Aerodynamics
Aerodynamic Analysis Under Influence of Heavy Rain, ICAS 2004-4.4.5 Aerodynamics
Aerodynamic Characteristics of Deflected Surfaces in Compressible Flows, ICAS 2004-3.6.2 Aerodynamics
Aerodynamic Design Optimization using Unstructured Navier-Stokes Equations Adjoint Method, ICAS 2004-2.7.5 Aerodynamics
Aerodynamic Efficiency of High Maneuverable Aircraft Applying Adaptive Wing Trailing Edge Section, ICAS 2004-4.3.2 Aerodynamics
AERODYNAMIC LOW SPEED BUFFET BOUNDARY CHARACTERISTICS OF A HIGH SPEED BUSINESS JET, ICAS 2004-4.4.R.1 Aerodynamics
Aerodynamic Optimization of Near-Sonic Plane Based on NEXST-1 SST Model, ICAS 2004-4.3.4 (St.) Aerodynamics
AERODYNAMIC STUDY OF A NOVEL TRAILING-EDGE FLAP CONCEPT OF A HIGH-LIFT TRANSPORT CONFIGURATION, ICAS 2004-3.11.2 Aerodynamics
Aircraft Design using a Gradient-Based Optimization Technique, ICAS 2004-2.5.2 Aerodynamics
An Analytical Approach to Trimming and Performance Coupling on Flying Wings, ICAS 2004-4.4.2 Aerodynamics
An Efficient Inverse Aerodynamic Design Method for Multi Component Devices, ICAS 2004-2.7.1 Aerodynamics
An Entropy Variable-Based Gridfree Euler Solver with LU-SGS Accelerator, ICAS 2004-2.4.3 Aerodynamics
An Evaluation Scheme for the Uncertainty Analysis of a Captive Trajectory System, ICAS 2004-2.10.1 Aerodynamics
An Experimental Study of a Retrorocket with a Cylindrical Body in Supersonic Free Streams, ICAS 2004-3.8.3 Aerodynamics
An Implicit Solution of the Unsteady Navier Stokes Equations on Unstructured Moving Grids, ICAS 2004-3.6.3 Aerodynamics
An Inverse Design Method for Engine Nacelles and Wings, ICAS 2004-2.7.2 Aerodynamics
An Overset Field-Panel Method for Unsteady Transonic Aeroelasticity, ICAS 2004-2.1.R.1 Aerodynamics
An Unsteady and Time-Averaged Study of a Ground Vortex Flow, ICAS 2004-2.9.R.1 Aerodynamics
Analysis and Modeling of Pressure Induced by Separated Reattaching Flows, ICAS 2004-3.9.4 Aerodynamics
Application of Pressure-Sensitive Paint to Low-Speed Wind Tunnel Testing at Japan Aerospace Exploration Agency, ICAS 2004-3.2.3 Aerodynamics
Applications of Underexpanded Jets in Hypersonic Aerothermodynamic Research, ICAS 2004-2.10.5 Aerodynamics
Applied CFD for Analyzing Aerodynamic Flows around Helicopters, ICAS 2004-6.11.1 Aerodynamics
BLEED PERTURBATION ACTIVE CONTROL OF FOREBODY ASYMMETRIC VORTICES, ICAS 2004-2.9.R.2 Aerodynamics
Boundary-Layer Transition Measurements on an Axisymmetric Body at Incidence at Supersonic Speed, ICAS 2004-3.3.3 Aerodynamics
CFD Analysis of Aerodynamic Heating for HYFLEX High Enthalpy Flow Tests and Flight Conditions, ICAS 2004-2.6.3 Aerodynamics
CFD Simulations of Aerodynamic Flows with a Pressure-Based Method, ICAS 2004-2.4.1 Aerodynamics
CFD Validation Study of NEXST-1 near Mach 1, ICAS 2004-2.3.R Aerodynamics
CFD-Based Aerodynamic Shape Optimization for Japanese Experimental Supersonic Transport, ICAS 2004-4.3.3 Aerodynamics
Characteristics of Wavepacket and Wedge-Shaped Disturbances Propagation in Supersonic Boundary Layer, ICAS 2004-3.5.1 Aerodynamics
Classification of Airfoils by Abnormal Behavior of Lift Curves at Low Reynolds number, ICAS 2004-3.10.2 Aerodynamics
Combined Probe for Mach Number, Temperature and Incidence Indication, ICAS 2004-3.1.1 Aerodynamics
Computational Analysis and Re-Design of a Wing-Strake Combination, ICAS 2004-4.3.1 Aerodynamics
Computational Study of Chemically Reacting Hypersonic Flow, ICAS 2004-3.7.4 (St.) Aerodynamics
Control of the Vortex Breakdown on a Delta Wing by Blowing, ICAS 2004-4.1.R.2 Aerodynamics
Curvature Effects in the Curved Duct for the Compressible Viscous Flow, ICAS 2004-3.6.1 (St.) Aerodynamics
Detection of Transition under Cryogenic Conditions using Temperature Sensitive Paint, ICAS 2004-3.2.1 Aerodynamics
Development of a 3-D Unstructured Grid Simulation Capability for Turbulent Aerospace Flows, ICAS 2004-2.6.2 Aerodynamics
Development of a Multi-Block/Overset Grid Solver, ICAS 2004-2.1.2 Aerodynamics
DEVELOPMENT OF A SIMPLE AND FAST COMPUTATIONAL ROUTINE TO SOLVE THE FULL POTENTIAL EQUATION OF THE TRANSONIC AXI- SYMMETRIC FLOW, ICAS 2004-2.4.R.4 Aerodynamics
Development of Multi-Disciplinary Simulation Codes and their Application for the Study of Future Space Transport Systems, ICAS 2004-2.6.4 Aerodynamics
DEVELOPMENT OF THE PRESSURE-SENSITIVE PAINT MEASUREMENT FOR LARGE WIND TUNNELS AT JAPAN AEROSPACE EXPLORATION AGENCY, ICAS 2004-3.2.2 Aerodynamics
Discontinous Galerkin Method for Duct Acoustics, ICAS 2004-3.4.2 Aerodynamics
Discrete Frequency Sound Radiation Due to Fluid Flow over Flat Plates with Acoustically Non-Compact Chord, ICAS 2004-P.5 Aerodynamics
Drag Reduction and Buffeting Alleviation in Transonic Periodic Flow over Biconvex Airfoils, ICAS 2004-3.9.3 Aerodynamics
Drag Reduction and Vortex Structure Modification in the Wake of a Circular Cylinder by Electrohydrodynamic Forces, ICAS 2004-3.9.R Aerodynamics
Effect of Stationary Vortex to Heat Transfer on Delta Wing, ICAS 2004-3.6.R Aerodynamics
Effects of Wingtip Geometry on Lift Distribution and Induced Drag, ICAS 2004-4.4.4 Aerodynamics
Estimation of Skin Surface Temperature of Space Vehicles During Whole Flight Envelope, ICAS 2004-3.7.R.2 Aerodynamics
EVALUATION OF THE RECURSIVE PROJECTION METHOD FOR EFFICIENT UNSTEADY TURBULENT CFD SIMULATIONS, ICAS 2004-2.1.1 (St.) Aerodynamics
EVALUATION OF TRANSONIC FLOW ANALYSIS AROUND ONERA MODEL M5 CONFIGURATION USING CASPER HYBRID UNSTRUCTURED NAVIER-STOKES CODE, ICAS 2004-P.20 Aerodynamics
Experimental Analysis of Aerodynamics Characteristics of Adaptive Multi-Winglets, ICAS 2004-2.11.2 Aerodynamics
Experimental Analysis of the Confluent Boundary Layer Between a Flap and a Main Element with Saw-Toothed Trailing Edge, ICAS 2004-2.10.R.1(St.) Aerodynamics
EXPERIMENTAL AND NUMERICAL CONFIGURATION STUDY ON UCAV’S AERODYNAMICS, ICAS 2004-P.7 Aerodynamics
Experimental Investigation of Rotor Vortex Wakes in Descent, ICAS 2004-2.9.3 (St.) Aerodynamics
Experimental Investigation of Spanwise Fences for Vortex Lift, ICAS 2004-2.9.1 Aerodynamics
Experimental Investigation of the Dynamic Stability Derivatives of a Fighter Model, ICAS 2004-2.10.2 Aerodynamics
EXPERIMENTAL INVESTIGATION OF THE EFFECT OF VARIOUS WINGLET SHAPES ON THE TOTAL PRESSURE DISTRIBUTION BEHIND A WING, ICAS 2004-2.11.3 Aerodynamics
Experimental Study on Hypersonic Heating Characteristics of Cavity Wake Flow, ICAS 2004-3.7.3 Aerodynamics
Experimental/Computational Collaboration in the Understanding of Boundary Layer Transition, ICAS 2004-3.3.1 (I.L.) Aerodynamics
Extra-Large Eddy Simulation for Delta-Wings and Space Launchers, ICAS 2004-2.8.1 Aerodynamics
Flow Over Thick Airfoils in Ground Effect - An Investigation on the Influence of Camber, ICAS 2004-P.11 Aerodynamics
Flow Visualization and PIV Measurements of Laminar Separation Bubble Oscillating at Low Frequency on an Airfoil near Stall, ICAS 2004-2.10.4 (St.) Aerodynamics
FLUCTUATING STATIC PRESSURE MEASUREMENTS IN THE ALLIED AEROSPACE NORTH AMERICAN 7 X 7 FOOT TRISONIC WIND TUNNEL, ICAS 2004-P.26 Aerodynamics
Grid Pattern Effects on Aerodynamic Characteristics of Grid Fins, ICAS 2004-2.11.R Aerodynamics
Heat Transfer with Ablation in Cylindrical Bodies, ICAS 2004-3.7.5 (St.) Aerodynamics
Hypervelocity Flow research in Ballistic Range, ICAS 2004-P.16 Aerodynamics
Identification of Tip-Jet Driven Rotor Noise using a Phased Microphone Array, ICAS 2004-3.4.4 Aerodynamics
Innovative High Lift Systems (IHK-HICON), ICAS 2004-3.11.1 (I.L.) Aerodynamics
Investigation of Rotor Noise Prediction Using Different Aeroacoustic Methods in Time Domain, ICAS 2004-3.4.R (St.).1 Aerodynamics
INVESTIGATION OF TRANSITION MODELLING FOR AEROFOIL DYNAMIC STALL, ICAS 2004-6.11.2 Aerodynamics
Kawasaki Wake Survey System, ICAS 2004-3.1.R.2 Aerodynamics
Laminar-Turbulent Transition Correlations in Supersonic / Hypersonic Flat Plate Flow, ICAS 2004-3.3.4 Aerodynamics
Low-Speed High-Lift Performance Improvements obtained and validated by the EC-project EPISTLE, ICAS 2004-4.1.1 Aerodynamics
Mach Wave Emission in a Plane Supersonic Jet at High Convective Mach Numbers, ICAS 2004-3.4.3 Aerodynamics
Mixed Element Type Unstructured Grid Generation and its Application to Viscous Flow Simulation, ICAS 2004-2.4 (St.).R.3 Aerodynamics
MODELING OF SPIN MODES OF SUPERSONIC AIRCRAFT IN HORIZONTAL WIND TUNNEL, ICAS 2004-3.1.4 Aerodynamics
Modification of Ordnance Release Characteristics for Transonic Shallow Cavities, ICAS 2004-4.2.1 Aerodynamics
Mutual Validation between EFD/CFD for Supersonic Flow around NEXST-1, ICAS 2004-2.6.1 Aerodynamics
NAL 60cm Magnetic Suspension and Balance System, ICAS 2004-3.1.2 Aerodynamics
Navier-Stokes Analysis for SCT Low-Speed High-Lift Flight and Wind Tunnel Configurations, ICAS 2004-4.1.2 Aerodynamics
Near Field Study of a Synthetic Jet, ICAS 2004-3.8.1 Aerodynamics
Nonequilibrium and Rarefaction Effects in the Hypersonic Multicomponent Viscous Shock Layers, ICAS 2004-3.7.1 Aerodynamics
Non-Linear Vortex Behaviors of Rolled Supersonic Transport Configuration with Leading-edge Vortex Flaps, ICAS 2004-4.1.3 Aerodynamics
Numerical Analysis of Free-to-roll Wing Rock Motion by the Fluid Dynamics-Flight Dynamics Coupling, ICAS 2004-2.2.1 Aerodynamics
Numerical Analysis of Interaction Noise Between Main Rotor and Tail Rotor of a Helicopter, ICAS 2004-6.11.3 Aerodynamics
Numerical Analysis Of Low Reynolds Number Flows around Thin Wings For Micro Air Vehicles, ICAS 2004-3.10.5 Aerodynamics
Numerical Analysis of the Oscillatory Behaviors of Supersonic Impinging Jet Flow, ICAS 2004-3.8.2 Aerodynamics
NUMERICAL INVESTIGATION OF BVI MODELING EFFECTS ON HELICOPTER ROTOR FREE WAKE SIMULATIONS, ICAS 2004-6.11.R.2 Aerodynamics
Numerical Prediction for Airfoil Stall, ICAS 2004-2.2.R.2 Aerodynamics
Numerical Prediction of Stagnation-Point Shock-Detachment Distance for Hypersonic Low Density Flow over Blunt Nose Shapes, ICAS 2004-3.7.R.1 Aerodynamics
Numerical Simulation around Wing Control Surfaces, ICAS 2004-2.3.2 Aerodynamics
Numerical Simulation of a Delta Wing with Vortex Breakdown using the Lattice Boltzmann Method, ICAS 2004-2.4.5 Aerodynamics
NUMERICAL SIMULATION OF FLOW FIELD IN AN ANNULAR TURBINE STATOR WITH FILM COOLING, ICAS 2004-2.6.R.2 Aerodynamics
Numerical Simulation of High Lift Configuration using Unstructured Mesh Method, ICAS 2004-2.3.4 Aerodynamics
Numerical Simulation of Supersonic Flowfield with Secondary Injection, ICAS 2004-3.6.4 Aerodynamics
NUMERICAL SIMULATION OF SUPERSONIC INTAKE USING STRUCTURED-UNSTRUCTURED ZONAL APPROACH, ICAS 2004-2.6.R.1 Aerodynamics
Numerical Study of High L/D Oblique Flying Wing, ICAS 2004-2.7 (St.).R.2 Aerodynamics
Numerical Study of Shock Generation at the After-Body of Slender Body Of Revolution using Navier-Stokes Equation, ICAS 2004-2.7.R.1 Aerodynamics
ON SOUND RADIATION FROM AN OPEN-ENDED NON-UNIFORMLY LINED CYLINDRICAL NOZZLE, ICAS 2004-P.25 Aerodynamics
ON THE APPLICATION OF TRANSITIONAL FLOW MODELS IN AIRFOIL COMPUTATIONS USING COUPLED NAVIER-STOKES AND e^N TRANSITION PREDICTION METHODS, ICAS 2004-2.8.3 Aerodynamics
On the Generation of Sound in a Shear Flow, ICAS 2004-3.4.5 Aerodynamics
ON THE RECEPTIVITY OF SUPERSONIC BOUNDARY LAYER TO OSCILLATING MACH WAVES, ICAS 2004-3.5.2 Aerodynamics
On the Shielding of Engine Noise by an Aircraft Wing, ICAS 2004-2.2.3 Aerodynamics
OPTWIN-a Constrained Numerical Optimization Method for Wing/Horizontal Tailplane Design, ICAS 2004-4.4.3 Aerodynamics
Parallel Chimera Computations of Helicopter Flows, ICAS 2004-6.11.R.1 Aerodynamics
Performance Improvement of Flush, Parallel Walled Auxiliary Intakes By Means of Vortex Generators, ICAS 2004-4.2.3 Aerodynamics
Performance of a Flapped Duct Exhausting into a Compressible External Flow, ICAS 2004-4.2.R.2 Aerodynamics
Reduced-Order Modeling of Unsteady Flows without Static Correction Requirement, ICAS 2004-2.1.4 Aerodynamics
Reynolds Number, Compressibility, and Leading-Edge Bluntness Effects on Delta-Wing Aerodynamics, ICAS 2004-4.1.4 Aerodynamics
Roll Damping Measurements of a Free Spinning Bomb, ICAS 2004-3.1.R.1 Aerodynamics
SMALL DISTURBANCE NAVIER-STOKES METHOD: AN EFFICIENT TOOL FOR PREDICTING UNSTEADY AIR LOADS, ICAS 2004-2.1.3 Aerodynamics
Stability of Supersonic Swept-Wing Boundary Layers with or without Crossflow, ICAS 2004-3.5.3 Aerodynamics
STEADY AND UNSTEADY CALCULATIONS ON FULL CONFIGURATION OF TWO-STAGE SPACE TRANSPORTATION SYSTEM DURING SEPARATION, ICAS 2004-2.2.2 Aerodynamics
Structure of Under Expanded Jet from Rectangular Nozzle, ICAS 2004-3.8 (St.).R Aerodynamics
Structured Multiblock Simulations of General Launcher Flows Including the Effect of Fins, ICAS 2004-2.3.3 Aerodynamics
STUDY OF THE EFFECTS OF SYNTHETIC JET ACTUATORS ON THE DELAY OF TRANSITION OF THE BOUNDARY LAYER DEVELOPED ON A FLAT PLATE, ICAS 2004-P.10 Aerodynamics
Study of Various Numerical Techniques for the Computation of Diffusive Terms in Two-dimensional Navier-Stokes Equations, ICAS 2004-2.4.R.1 Aerodynamics
TBD, ICAS 2004-3.11.3 Aerodynamics
The Aerodynamic Performance of Thrust Reverser cascade, ICAS 2004-4.2.R.1 Aerodynamics
The Concept of High-Lift, Mild Stall Wing, ICAS 2004-3.10.4 Aerodynamics
The Global Stability Analysis of Laminar Separation Flow over an Airfoil, ICAS 2004-3.3.2 Aerodynamics
The Influence of Streamwise Modulation on the Evolution of Three-Dimensional Wavetrains in Boundary Layers, ICAS 2004-3.3.R Aerodynamics
The Intake-Duct Flow Correction by CFD for Jet-Powered Supersonic Experimental Airplane Wind Tunnel Test Data, ICAS 2004-2.10.R.2 Aerodynamics
The New Closed Circuit Wind Tunnel of the Aircraft Laboratory of Univ. of São Paulo, Brazil, ICAS 2004-P.2 Aerodynamics
The Properties of Wing and Airflow of Flying Insects, ICAS 2004-3.10.1 Aerodynamics
The Use of Unsteady CFD Data on Aeroelastic Analysis for Generic Large Transport Aircraft, ICAS 2004-2.1.R.3 Aerodynamics
Three Dimensional Boundary Layer Transition Analysis in Supersonic Flow Using a Navier-Stokes Code, ICAS 2004-2.8.2 Aerodynamics
THREE-DIMENSIONAL MULTIOBECTIVE CONSTRAINED OPTIMIZATION OF AERODYNAMIC SHAPES, ICAS 2004-2.7.3 Aerodynamics
Turbulent Forced Convective Heat Transfer, ICAS 2004-3.5 (St.).R Aerodynamics
UNSTEADY AERODYNAMICS OF FLAPPING WINGS, ICAS 2004-3.10.3 (St.) Aerodynamics
UNSTEADY BEHAVIOR OF LEADING-EDGE VORTEX AT STATIC AND DYNAMIC MODEL CONDITIONS, ICAS 2004-2.9.2 Aerodynamics
Validation of Wing Technologies on an Airbus A 340 Flying Testbed: First Flight Test Results from the European Program AWIATOR, ICAS 2004-4.4.1 (I.L.) Aerodynamics
Vortex Behaviors over a Cranked Arrow Wing Configuration at High Angles of Attack, ICAS 2004-2.9.4 Aerodynamics
Vortex Interaction and Breakdown of a Double-Delta Wing at Sideslip, ICAS 2004-4.1.R.1 Aerodynamics
Wall Measurements in a Cavity Flow, ICAS 2004-3.4.R.2 Aerodynamics
Wind Tunnel Wall Boundary Layer Control for 2D High-Lift Wing Testing, ICAS 2004-2.10.3 Aerodynamics
Agent-Based Modeling and Experimentation for Real-Time Collaborative Decision Making in Air Traffic Management, ICAS 2004-8.2.2 Air Transport System Efficiency
Airborne-Managed Spacing in Multiple Arrival Streams, ICAS 2004-8.5.2 (I.L.) Air Transport System Efficiency
Conflict Detection and Alerting in a Self Controlled Terminal Airspace, ICAS 2004-8.2.3 (I.L.) Air Transport System Efficiency
CONFLICT DETECTION AND ALERTING IN A SELF CONTROLLED TERMINAL AIRSPACE, ICAS 2004-8.4.R.2 (I.L.) Air Transport System Efficiency
Design of Tunnel-in-the-Sky Display and Curved Trajectory, ICAS 2004-8.4.4 Air Transport System Efficiency
Development and Evaluation of an Airborne Separation Assurance System for Autonomous Aircraft Operations, ICAS 2004-8.4.1 (I.L.) Air Transport System Efficiency
FOUNDATION FOR STUDY OF FUTURE TRANSPORTATION SYSTEMS THROUGH AGENT-BASED SIMULATION, ICAS 2004-8.1.3 Air Transport System Efficiency
Integration of Paired-Dependent Speed Guidance into Current-Generation Glass-Cockpit Commercial Aircraft, ICAS 2004-8.3.3 (I.L.) Air Transport System Efficiency
Intermodality from a Passenger Perspective, ICAS 2004-8.5.3 (St.) Air Transport System Efficiency
Performance Analysis of a Conflict Probe Utilizing Only State Vector Information, ICAS 2004-8.4.3 Air Transport System Efficiency
Pilot In Command: A Feasibility Assessment of Autonomous Flight Management Operations, ICAS 2004-8.2.1 (I.L.) Air Transport System Efficiency
Practical Examples of Procedure Development for Unmanned Flight in Controlled Airspace, ICAS 2004-8.4.2 Air Transport System Efficiency
Preliminary Validation of the Small Aircraft Transportation System Higher Volume Operations (SATS HVO) Concept, ICAS 2004-8.1.R Air Transport System Efficiency
Preliminary Validation of the Small Aircraft Transportation System Higher Volume Operations (SATS HVO) Concept, ICAS 2004-8.5.1 (I.L.) Air Transport System Efficiency
RUNWAY CAPACITY PLANNING SUPPORTED BY DYNAMIC PROGRAMMING, ICAS 2004-8.3.4 Air Transport System Efficiency
SCALE-FREE NETWORKS AND COMMERCIAL AIR CARRIER TRANSPORTATION IN THE UNITED STATES, ICAS 2004-8.3.2 (I.L.) Air Transport System Efficiency
Technologies and Advanced Operations to Enhance Capacities throughout the Air Transport System, ICAS 2004-8.3.1 Air Transport System Efficiency
The Future Air Transport System in Europe: Vision and Perspectives, ICAS 2004-8.1.1 (I.L.) Air Transport System Efficiency
Transforming the NAS: The Next Generation Air Traffic Control System, ICAS 2004-8.1.2 (I.L.) Air Transport System Efficiency
A New Positioning/Navigation System Based on Pseudolites Installed on High Altitude Platforms Systems (HAPS), ICAS 2004-P.32 Aircraft and Systems Integration
A New UAV after Federica, ICAS 2004-1.10.3 Aircraft and Systems Integration
A Vision for the Future Evolution of Aircraft, ICAS 2004-1.2.R Aircraft and Systems Integration
Advanced Combat Aircraft Design For Low Support Cost, ICAS 2004-1.1.R Aircraft and Systems Integration
An Initial Design Methodology for Operational Hypersonic Military Aircraft, ICAS 2004-1.1.2 Aircraft and Systems Integration
AUTOMATION OF PRE-MISSION SUCCESS EVALUATION MODULE FOR MEDICAL EMERGENCY HELICOPTERS OPERATIONS, ICAS 2004-1.9.R Aircraft and Systems Integration
Close Proximity Dynamic Derivatives, ICAS 2004-1.4.2 Aircraft and Systems Integration
Conceptual Design and Feasibility for a Miniature Mars Exploration Rotorcraft, ICAS 2004-1.8.2 (St.) Aircraft and Systems Integration
Conceptual Feasibility of Flight Demonstrator, ICAS 2004-1.11.R.1 Aircraft and Systems Integration
Conceptual Study of a Supersonic Low Observable Heavy Ground Attack Missile, ICAS 2004-1.5.2 Aircraft and Systems Integration
Configuration Analysis of a Torqueless Helicopter Concept, ICAS 2004-1.9.4 Aircraft and Systems Integration
Crew Capability Evaluation in Helicopter Emergency Medical Service Operations: Operator Inputs, ICAS 2004-P.27 Aircraft and Systems Integration
Delta Wing with Leading Edge Extension and Propeller Propulsion for Fixed Wing MAV, ICAS 2004-1.10.5 Aircraft and Systems Integration
Design of a Low-Cost Easy-to-Fly Ultralight Aircraft in Composite Material, ICAS 2004-P.33 Aircraft and Systems Integration
Design of an Advanced Ground Station for Simultaneous Control of Multiple UAVs in a Coordinated Mission, ICAS 2004-1.8.3 Aircraft and Systems Integration
Design of Multi-Lifting Surfaces at Transonic Flow, ICAS 2004-1.5.3 Aircraft and Systems Integration
Development Approach to the PW_103 - An Increased Reliability Male UAV - Under the CAPECON Project within the V FR of EU, ICAS 2004-1.6.R.2 Aircraft and Systems Integration
Development of the Honda Jet, ICAS 2004-1.7.2 (I.L.) Aircraft and Systems Integration
Evolution in the design of the modern rigid hang glider, ICAS 2004-P.6 Aircraft and Systems Integration
Feasibility Study of a Technological Demonstrator of Reduced Size for Sub-orbital Fight, ICAS 2004-1.11.2 Aircraft and Systems Integration
FLYING WINGS AND EMERGING TECHNOLOGIES: AN EFFICIENT MATCHING, ICAS 2004-1.3.2 Aircraft and Systems Integration
Future Inter-theatre Multi-role Aircraft Concept, ICAS 2004-1.8.R Aircraft and Systems Integration
HALE UAV Platform Optimized for a Specialized 20-km Altitude Patrol Mission, ICAS 2004-1.6.3 Aircraft and Systems Integration
HISTORY OF UAV DEVELOPMENT IN IAI & ROAD AHEAD, ICAS 2004-1.6.1 (I.L.) Aircraft and Systems Integration
Integration of a Scenario Method in AIRBUS' Technology and Project Evaluation, ICAS 2004-1.1.3 Aircraft and Systems Integration
INTEGRATION OF SURVIVABILITY ASSESSMENT INTO COMBAT AIRCRAFT DESIGN FOR OPERATIONAL EFFECTIVENESS, ICAS 2004-1.5.1 Aircraft and Systems Integration
It takes more than Science, ICAS 2004-1.7.3 (I.L.) Aircraft and Systems Integration
MOB – A EUROPEAN PROJECT ON MULTIDISCIPLINARY DESIGN OPTIMISATION, ICAS 2004-1.3.4 (I.L.) Aircraft and Systems Integration
Modeling Upgrade Design of Maritime Helicopters for Anti-Submarine Missions – Automation Process, ICAS 2004-P.21 Aircraft and Systems Integration
Modern LTA Flight Vehicle: An Aerospace Platform for the Next Century?, ICAS 2004-P.23 Aircraft and Systems Integration
Multi-disciplinary Aircraft Design Optimization using Parallel Computer Architectures, ICAS 2004-1.4.R.2 Aircraft and Systems Integration
Multidisciplinary Optimization of Space Plane Modeled as Rigid Body, ICAS 2004-1.4.4 (St.) Aircraft and Systems Integration
Multi-mission Unmanned Aerial Vehicle Concept: Modeling Status, ICAS 2004-1.10.4 Aircraft and Systems Integration
MULTIOBJECTIVE AIRCRAFT DESIGN OPTIMIZATION FOR LOW NOISE AND EMISSIONS, ICAS 2004-1.4.3 Aircraft and Systems Integration
New Rotorcraft Design Criteria for Maximized Performance at Minimized Vibratory Loads, ICAS 2004-1.9.3 Aircraft and Systems Integration
Overview of Boeing BWB, ICAS 2004-1.3.1 (I.L.) Aircraft and Systems Integration
PASSENGER ACCEPTANCE OF BWB CONFIGURATIONS, ICAS 2004-1.3.3 Aircraft and Systems Integration
Performance Analysis of UAV-Interceptor, ICAS 2004-1.6.4 Aircraft and Systems Integration
Performance and Viability Study of an Amphibious Light Aircraft, ICAS 2004-1.2.3 Aircraft and Systems Integration
Progress Toward Integrated Vehicle Design for Hypersonic Systems, ICAS 2004-1.4.1 Aircraft and Systems Integration
Recent Advances in Air-vehicle Design Synthesis and Optimisation, ICAS 2004-1.1.1 Aircraft and Systems Integration
Recent Research Programs of the MuPAL-e Research Helicopter, ICAS 2004-1.9.2 Aircraft and Systems Integration
Small Aircraft Transportation Systems Project, ICAS 2004-1.7.5 (I.L.) Aircraft and Systems Integration
Staging of Two-Stage-to-Orbit Aerospace Plane, ICAS 2004-1.11.1 Aircraft and Systems Integration
SUITABILITY OF FUTURE TRANS-ATMOSPHERIC VEHICLES FOR MASS SPACE TOURISM FLIGHTS, ICAS 2004-1.11.3 Aircraft and Systems Integration
System Decomposition Method Based on Pareto and the Application to the Optimization of the Aircraft Configuration Design, ICAS 2004-1.4.5 Aircraft and Systems Integration
TACOM - Air-Launched Multi-Role UAV, ICAS 2004-1.10.1 Aircraft and Systems Integration
Tail-Sitter VTOL-UAV ~ Full-Scale Hover Prototype System, ICAS 2004-1.6.R.1 Aircraft and Systems Integration
Tail-Sitter VTOL-UAV Research Project Overview, ICAS 2004-1.6.2 Aircraft and Systems Integration
TBD, ICAS 2004-1.7.4 (I.L.) Aircraft and Systems Integration
Technological Challenges for Future Business Jets, ICAS 2004-1.7.1 (I.L.) Aircraft and Systems Integration
The Airbus / Engine & Nacelle Manufacturers relationship: Towards a more integrated, environmentally friendly engineering design, ICAS 2004-1.4.R.1 Aircraft and Systems Integration
The Continuation Design Framework for Nonlinear Entomopter Control, ICAS 2004-1.10.2 Aircraft and Systems Integration
The Evolution of the Tiltrotor - From Dream to Reality, ICAS 2004-1.9.1 Aircraft and Systems Integration
THE ORNICOPTER: A SINGLE ROTOR WITHOUT REACTION TORQUE, BASIC PRINCIPLES, ICAS 2004-1.8.1 Aircraft and Systems Integration
Twin-Fuselage Giant Seaplane Transport, ICAS 2004-1.2.2 Aircraft and Systems Integration
UCAVs moves toward revolution in future war time, ICAS 2004-P.15 Aircraft and Systems Integration
Uses of CAD Tools for Weight Estimation in Aircraft Conceptual Design, ICAS 2004-1.1.4 Aircraft and Systems Integration
X-31 VECTOR: Overview of Program and Results, ICAS 2004-1.2.1 (I.L.) Aircraft and Systems Integration
Collaborative European Aero-engine Environmental Research Programmes led by Snecma and Rolls-Royce, ICAS 2004-6.9.1 (I.L.) Challenge of the Environment
ENVIRONMENTAL CONSTRAINTS AND APPROPRIATE R&D STRATEGY FOR COMBUSTOR TECHNOLOGY, ICAS 2004-6.9.3 (I.L.) Challenge of the Environment
Integrated active systems for Aircraft interior noise control, ICAS 2004-6.10.5.R.3 Challenge of the Environment
Interior noise predection for generic CFRP and metal fuselages, ICAS 2004-6.10.5.R.2 Challenge of the Environment
Low Emissions Propulsion Engine Combustor Technology Evolution Past, Present and Future, ICAS 2004-6.9.2 (I.L.) Challenge of the Environment
NASA’S QUIET AIRCRAFT TECHNOLOGY PROJECT, ICAS 2004-6.10.1 (I.L.) Challenge of the Environment
Noise Saving Potential of Future Approach and Departure Procedure, ICAS 2004-6.10.3 Challenge of the Environment
Piezoelectric actuated flaps for active rotor control, ICAS 2004-6.10.5.R.1 Challenge of the Environment
Prediction of Stratospheric Ozone Change due to Nitrogen Oxides in Exhaust of Supersonic Airplane, ICAS 2004-6.9.4 Challenge of the Environment
Silencer Program, ICAS 2004-6.10.2 (I.L.) Challenge of the Environment
STUDY OF SSBJ NOISE REDUCTION WITH RATIONAL AIRCRAFT AND ENGINE CONTROL, ICAS 2004-6.10.4 Challenge of the Environment
The Contribution of the Air Transport Sector on The Atmospheric Pollution of Greater Athens Area, ICAS 2004-6.9.R Challenge of the Environment
The Zero Splice Engine Intake Liner: an Efficient Way of Reducing Aircraft Noise Without any Weight or Aerodynamic Penalty, ICAS 2004-6.10.5 Challenge of the Environment
A Polytopic Model of Aircraft and Gain Scheduling State Feedback Control, ICAS 2004-7.2.2 Flight Dynamics and Control
A Simplified Hazard Area Prediction (SHAPe) Model for Wake Vortex Encounter Avoidance, ICAS 2004-4.6.4 Flight Dynamics and Control
Aeroservoelastic Stability of Guided Missiles, ICAS 2004-8.11.R.1 Flight Dynamics and Control
Aircraft control using the engines (JET PROPULSION SYSTEMS), ICAS 2004-8.11.R.2 Flight Dynamics and Control
Aircraft Fault Detection and Isolation Using Disturbance Accommodation Technique, ICAS 2004-4.8.3 Flight Dynamics and Control
An Approximate Solution of 3D Variable Speed Interception Games, ICAS 2004-4.7.5 Flight Dynamics and Control
An Off-line Clearance Approach Using Bifurcation Analysis Methods In Support Of Flight Test, ICAS 2004-4.10.5 Flight Dynamics and Control
Analysis of Approximation of Aircraft Stochastic Motion by Markov Model, ICAS 2004-4.10.2 Flight Dynamics and Control
Audiovisual Flight Advisory System, ICAS 2004-4.6 (St.).R Flight Dynamics and Control
Automatic Take-off and Landing System for Fixed Wing Small Aircraft, ICAS 2004-4.9.2 Flight Dynamics and Control
Autonomous Flight Control and Guidance System of Accident Aircraft, ICAS 2004-4.6.2 Flight Dynamics and Control
Comparison and Improvement of Methods to Solving the Problem of Optimal Flight Routing, ICAS 2004-4.7.4 (St.) Flight Dynamics and Control
Control Allocation and Autopilot Design for Agile Missile, ICAS 2004-7.1.3 (St.) Flight Dynamics and Control
Data-Based Nonlinear Aeroelastic Modeling, ICAS 2004-8.11.3 Flight Dynamics and Control
Design and Evaluation of TACOM Control Logics, ICAS 2004-7.1.2 Flight Dynamics and Control
Design of a Robust LPV Control System for an Unmanned Observation Blimp, ICAS 2004-7.3.4 (St.) Flight Dynamics and Control
Development of an autonomous Micro Aerial Vehicle (MAV), ICAS 2004-7.3.3 Flight Dynamics and Control
Evaluation of Self-Repairing Flight Control System by Dynamic Free-Flight Wind-Tunnel Test, ICAS 2004-4.10.4 Flight Dynamics and Control
Experimental and Theoretical Studies of Autogyro Fight Dynamics, ICAS 2004-4.10.3 Flight Dynamics and Control
Flight Controller Design via a New Method to Estimate Work Load Levels, ICAS 2004-7.2.3 (St.) Flight Dynamics and Control
Flight Experiment on a Flight Path Optimization Algorithm for Aircraft in Trouble, ICAS 2004-4.6.3 Flight Dynamics and Control
Genetic Algorithm Technique Applied to a Forced Landing Manoeuvre, ICAS 2004-8.11.2 Flight Dynamics and Control
High Speed Flight Demonstration Project, ICAS 2004-7.1.1 (I.L.) Flight Dynamics and Control
Highly Reliable Flight Control System Design for Autonomous Flight Vehicles, ICAS 2004-4.8.2 Flight Dynamics and Control
INFLIGHT SIMULATION OF SUSTAINED HIGH ROLL RATES USING A LOW ALPHA SPIN MODE: POTENTIAL APPLICATION TO AVIATION MEDICINE RESEARCH, ICAS 2004-8.11.1 Flight Dynamics and Control
Initial Flight Testing of the HondaJet, ICAS 2004-4.10.1 (I.L.) Flight Dynamics and Control
INITIAL VERIFICATION OF A 3D MORPHOGENETIC MODEL OF IN-FLIGHT ICING ON A CYLINDER, ICAS 2004-P.19 Flight Dynamics and Control
Large-Scale Air-Combat Formation Optimization using Simulated-Annealing GA (Genetic Algorithm), ICAS 2004-4.7.2 (St.) Flight Dynamics and Control
Lateral Autopilot Design for a UAV Using Coefficient Diagram Method, ICAS 2004-7.3.2 Flight Dynamics and Control
MINIMUM UNSTICK SPEED CALCULATION FOR HIGH-SPEED JET TRANSPORT AIRCRAFT, ICAS 2004-4.9.3 Flight Dynamics and Control
Modelling Response of Flexible High Aspect Ratio Wings to Wind Turbulence, ICAS 2004-4.6.1 (I.L.) Flight Dynamics and Control
Modified Proportional Navigation for a Missile with Varying Velocity - Comparison with the Optimal Guidance, ICAS 2004-4.11.3 Flight Dynamics and Control
New General Approach to the Airplane Rotation Analysis, ICAS 2004-4.9.1 Flight Dynamics and Control
New Possibilities of Significant Improvement of Aerospace Launcher Efficiency by Rigorous Optimization of Atmospheric Flight, ICAS 2004-4.7.1 (I.L.) Flight Dynamics and Control
Nonlinear Model Matching Flight Control System for Lift/Cruise Fan Aircraft, ICAS 2004-7.2.R Flight Dynamics and Control
OPTIMIZATION OF HIGH ANGLE-OF-ATTACK APPROACH AND LANDING TRAJECTORIES, ICAS 2004-4.7.3 Flight Dynamics and Control
PARAMETER ESTIMATION AND FLIGHT PATH RECONSTRUCTION USING OUTPUT-ERROR METHOD, ICAS 2004-4.11.1 Flight Dynamics and Control
Performance Calculations of Autogyro, ICAS 2004-4.9.4 (St) Flight Dynamics and Control
Preliminary Exploration of Evaluation Trial Flight Test of the Commanding Control System ......, ICAS 2004-P.18 Flight Dynamics and Control
Real Time Prediction of ship motions and attitudes using advanced prediction techniques, ICAS 2004-P.30 Flight Dynamics and Control
ROBUST CONTROL AND CLOSED-LOOP IDENTIFICATION BY NORMALIZED COPRIME FACTORIZATION, ICAS 2004-4.11.2 Flight Dynamics and Control
Robust Control of the Aircraft-on-ground Lateral Motion, ICAS 2004-7.2.1 Flight Dynamics and Control
Six Components of Aerodynamic Forces and Moments of Free Flight Airplane Model in Wind Tunnel Measured by Single Video Camera, ICAS 2004-4.10.R Flight Dynamics and Control
THE RESEARCH ON IR IMAGING TERMINAL-GUIDING TECHNOLOGY FOR AN AIR-TO-AIR MISSILE IN CLUTTER BACKGROUND, ICAS 2004-7.1.R Flight Dynamics and Control
Tools for Flight Dynamics Analysis in the Design of MAVs, ICAS 2004-7.3.1 (I.L.) Flight Dynamics and Control
TP MODEL TRANSFORMATION IN NONLINEAR CONTROL DESIGN, ICAS 2004-4.8.1 (I.L.) Flight Dynamics and Control
Viable Feedback Space Trajectory Control, ICAS 2004-7.1.4 Flight Dynamics and Control
Bigger, faster, greener, cheaper? Developing the AIRBUS response to the Vision 2020 demands, ICAS 2004-0.3: GENERAL LECTURE II: General Lecture
Innovation in Aerospace & Defence Industry - A European/US perspective, ICAS 2004-0.4: GENERAL LECTURE III: General Lecture
PERSPECTIVES OF FUTURE DEVELOPMENTS OF VERTICAL FLIGHT: The Point Of View Of Industry, ICAS 2004-0.2: GENERAL LECTURE I: General Lecture
Transformations in Air Transportation Systems for the 21st Century, ICAS 2004-0.5: GENERAL LECTURE IV: General Lecture
Progress and Future Prospects of CFD in Aerospace: Observations from 30 years Research, ICAS 2004-0.1: ICAS DANIEL & FLORENCE GUGGENHEIM MEMORIAL LECTURE: ICAS DANIEL & FLORENCE GUGGENHEIM MEMORIAL LECTURE
A Flutter Model for Rotor Blades with Flaps, ICAS 2004-5.8.1 (I.L.) Materials and Structures
A New Approach to Evaluate Durability and Damage Tolerance for Aircraft Composite Structures, ICAS 2004-5.3.3 Materials and Structures
Advanced Materials and Coatings for Future Gas Turbine Applications, ICAS 2004-5.5.1 (I.L.) Materials and Structures
Aeroelastic Modeling of Vertical Tail Buffet, ICAS 2004-5.7.R Materials and Structures
Aircraft Equivalent Vulnerable Area Calculation Methods, ICAS 2004-5.6 (St.).R.2 Materials and Structures
Amendment of High-Altitude Corrosion Environment to the Fatigue Life of Aircraft, ICAS 2004-P.3 Materials and Structures
AN IMPROVED LONG LIFE DURATION CERAMIC MATRIX COMPOSITE MATERIAL FOR JET AIRCRAFT ENGINE APPLICATIONS, ICAS 2004-8.9.1 Materials and Structures
An Investigation of the Effects of Ageforming on the Microstructure in Aerospace Alloys, ICAS 2004-5.6.1 (St.) Materials and Structures
Analysis and Rig Test in EMB170 Flap Mechanism Development, ICAS 2004-P.8 Materials and Structures
Application of Quantitative Microfractography in Damage Tolerance and Fatigue Evaluation of Wing Spar, ICAS 2004-5.6.4 Materials and Structures
COMPOSITE LANDING GEAR COMPONENTS FOR AEROSPACE APPLICATIONS, ICAS 2004-5.3.2 Materials and Structures
Computer Simulation of Effects of Refiners on Cast Grain Structures of Superalloy K4169, ICAS 2004-P.1 Materials and Structures
CONTINUOUS DYNAMIC RECRYSTALLIZATION OF EXTRUDED NIAL POLYCRYSTALS DURING SUPERPLASTIC DEFORMATION PROCESS, ICAS 2004-8.9.2 Materials and Structures
Controlling Linear Flexible Systems Dynamics by Using Active Control with Optimal Control Theory, ICAS 2004-P.24 Materials and Structures
Correction of Flutter Boundary of Non-Planar Wing Using Measured Local Mach Number, ICAS 2004-5.7.1 Materials and Structures
Design and Experimental Application of Mixed LPV/ Controller for Active Flutter Suppression, ICAS 2004-5.8.3 Materials and Structures
Development of Micro Spark Coating, ICAS 2004-5.5.2 Materials and Structures
Development of Safe, Environmentally Friendly Airplane Seat Cushions, ICAS 2004-5.9.R.3 Materials and Structures
Dynamic Buckling Tests of Cylindrical Shells in Composite Materials, ICAS 2004-5.3.4 Materials and Structures
Effects of Physical and Chemical Aging on Strength and Behavior of Carbon/BMI Composites for SST Structures, ICAS 2004-5.9.1 (I.L.) Materials and Structures
EMBRAER170 Wing Bird Strike Test, ICAS 2004-5.10.R.2 Materials and Structures
Experimental and Theoretical System Identification of Flexible Structures with Piezoelectric Actuators, ICAS 2004-5.1.2 Materials and Structures
FATIGUE MONITORING AND OPERATIONAL SAFETY IMPROVEMENT OF SMALL SPORT PLANES, ICAS 2004-5.4.5 Materials and Structures
FATIGUE STRENGTH OF AL-ALLOYS IN CASE OF RANDOM SPECTRA LOADING, ICAS 2004-5.4.2 Materials and Structures
FEM ANALYSIS OF INTERNAL STRESS SUPERPLASTICITY IN AL/SICW COMPOSITE WITH DIFFERENT VF SUBJECTED TO THERMAL CYCLING, ICAS 2004-5.5.3 Materials and Structures
FEM Based Bending Analyses of Stiffened Composite Panels, ICAS 2004-4.5.1 Materials and Structures
Flutter Control of Wind Tunnel Model Using a Single Element of Piezo-Ceramic Actuator, ICAS 2004-5.7.3 (St.) Materials and Structures
Improvement of Interlaminar Strength on CFRP Laminates by Carbon Fiber Stitching, ICAS 2004-5.9.4 Materials and Structures
INFLUENCE OF THE DIAMETER OF TYRANNO ZMI FIBER ON THE STATISTICAL STRENGTH, ICAS 2004-5.9 (St).R.2 Materials and Structures
Influence of the Store on the Transonic and Supersonic Flutter Characteristics of a Delta Wing Configuration, ICAS 2004-5.10.4 Materials and Structures
Mathematical Model Improvement for the Nonlinear Characteristics of Transonic Flutter, ICAS 2004-5.7.2 (St.) Materials and Structures
Model Order Reduction for Aeroservoelasticity Studies by use of LRSRM and LRSM Algorithms, ICAS 2004-5.7.5 Materials and Structures
Modeling the Low Velocity Impact Response of aa Aerospace Composite Replacement Panel, ICAS 2004-5.2.3 Materials and Structures
MSD Simulation in Lap Joints Using a DBEM Model, ICAS 2004-5.4.1 (I.L.) Materials and Structures
Multi Objective Design Study of a Flapping Wing Generator, ICAS 2004-5.2 (St.).R Materials and Structures
Multilevel Distributed Substructure Optimization, ICAS 2004-4.5.3 Materials and Structures
NATURAL FREQUENCIES OF ROTATING CANTILEVER FLEXIBLE BEAMS BY USING THE p-VERSION OF THE FINITE ELEMENT METHOD, ICAS 2004-P.17 Materials and Structures
NATURAL FREQUENCY RESPONSE OF RIGID, CELLULAR SUPPORTED COMPOSITE PLATES, ICAS 2004-5.11.3 Materials and Structures
New Composite Design and manufacturing Methods for General Aviation Aircraft Structures, ICAS 2004-5.3.1 (I.L.) Materials and Structures
New Diagnostic System to Assess the Technical State of Objects Operating in a Fatigue Environment, ICAS 2004-5.4.3 Materials and Structures
Non-Homogeneous Composite Beams: Analytic Formulation and Solution, ICAS 2004-4.5.2 Materials and Structures
Non-Linear Vibration and Damping Characterizations of Delaminated Composite Laminates by Using Multilayered Finite Elements, ICAS 2004-5.2.2 Materials and Structures
Novel Liquid Crystal Thermoset Resins for Cryogenic Fuel Tank Applications, ICAS 2004-5.9.2 Materials and Structures
Numerical Analysis of Damping Enhancement of a Beam with Shape Memory Alloy Foils Bonded, ICAS 2004-5.2.1 (I.L.) Materials and Structures
NUMERICAL AND EXPERIMENTAL SIMULATION OF DAMAGE BEHAVIOUR OF FIBRE METAL LAMINATES, ICAS 2004-5.6.2 Materials and Structures
Operational Load Regression Equation Development for Advanced Fighter Aircraft, ICAS 2004-5.4.R.2 Materials and Structures
OPTIMIZATION FOR COMPOSITE WING USING GENETIC ALGORITHM AND GRID TECHNOLOGY, ICAS 2004-5.8.2 Materials and Structures
Optimum Structural and Topological Optimization Using an Improved Method of Simulated Annealing, ICAS 2004-P.22 Materials and Structures
POSSIBLE DECREMENT OF LCO FLUTTER DYNAMIC PRESSURE DUE TO ROBUST CONTROLLER, ICAS 2004-5.10.3 Materials and Structures
Preliminary Study of Non-Linear Aeroelasticity in Hypersonic Flow, ICAS 2004-5.7.4 (St.) Materials and Structures
Processing and Properties of New High Temperature Composites Using Superior Polyimide "Tri-A PI", ICAS 2004-5.9.R.1 Materials and Structures
RESIDUAL STRENGTH ANALYSIS OF STIFFENED PANELS USING R-CURVES OF SKIN MATERIAL, ICAS 2004-5.6.R.1 Materials and Structures
Residual Strength Prediction of Impact Damaged, ICAS 2004-5.3.R.1 Materials and Structures
Rotor Blade Air Loads EvaluationBased on Structural Deformation, ICAS 2004-5.1.R.1 Materials and Structures
SIMULATION OF AIRCRAFT LANDING GEAR DYNAMICS USING FLEXIBLE MULTIBODY DYNAMICS METHODS IN SIMPACK, ICAS 2004-5.1.4 Materials and Structures
State Space Reconstruction of Non-Linear Stall-Induced Oscillatory Aeroelastic Motion, ICAS 2004-5.10.5 Materials and Structures
Status and Summary of Test Method Standardization of Advanced Composites in Japan, ICAS 2004-5.9.3 Materials and Structures
Steady-state Creep Rate - A Mythical Fundamental Property, ICAS 2004-8.9.3 Materials and Structures
Strain Gage Loads Calibration Parametric Study, ICAS 2004-5.4.4 Materials and Structures
The Behavior of Rubber During Pressure Forming of Thermoplastic Composites, ICAS 2004-5.5 (St.).R.1 Materials and Structures
The Influence of Material and Geometric Non-Linearities to Accuracy FEM Stress Analysis of Landing Gear, ICAS 2004-5.1.1 Materials and Structures
The Size Effect of SiC Fiber Strength on the Gauge Length, ICAS 2004-8.9.4 (St.) Materials and Structures
The Static Strength Analysis of Friction Stir Welded Stiffened Panels for Primary Fuselage Structure, ICAS 2004-5.6.3 Materials and Structures
Thermal Conductivity Measurement of Thermal Insulation under High Temperature, ICAS 2004-8.9.R Materials and Structures
Thermally Induced Vibration Control of Composite Thin-Walled Rotating Blade, ICAS 2004-5.1.3 Materials and Structures
TIME-ACCURATE SIMULATION OF A MANOEUVRING AEROELASTIC DELTA WING AT HIGH ANGLE OF ATTACK, ICAS 2004-5.10.1 Materials and Structures
Toughness Improvement of Glass/Epoxy Filament Wound Tubes by Rubber Modification, ICAS 2004-5.5.R.2 Materials and Structures
Transonic and Supersonic Aeroelastic Computation Considering, ICAS 2004-5.10.R.1 Materials and Structures
Two-level Scheme for Selection of Degrees of Freedom by Energy Estimation Combined with Sequential Elimination, ICAS 2004-5.11.1 Materials and Structures
Use of Aeroelasticity; Multidisciplinary Investigation, ICAS 2004-5.10.2 Materials and Structures
Vibration and Position Control of Micro/Macro Hybrid Manipulator System, ICAS 2004-5.11.2 Materials and Structures
Virtual Testing of Aircraft Fuselage Stiffened Panels, ICAS 2004-5.4.R.1 Materials and Structures
Weight Estimation of Composite Secondary Structure, ICAS 2004-5.1.R.2 Materials and Structures
A Comparative Analysis of the Aerodynamic Characteristics of Two Configurations of Nacelle on a Light Twin-Engine Aircraft Wing-Body, ICAS 2004-6.3.2 Propulsion
Aerodynamic Analysis of Propeller-Wing Interaction for the Development of a Custer Channel Wing, ICAS 2004-6.3.R Propulsion
Aerodynamic Performances of the Combined Cycle Inlet, ICAS 2004-6.6.1 Propulsion
An Evaluation of a Hydrogen Peroxide-Based Bi-Propellant Gas Generator for an Advanced Air Turbo Ramjet, ICAS 2004-6.4.5 Propulsion
Common Solutions to Commercial and Military Propulsion Requirements, ICAS 2004-6.4.1 Propulsion
CONCEPTUAL DESIGN FOR A SUAV PROPULSION SYSTEM SIZING, ICAS 2004-6.3.4 Propulsion
Conjugate Heat Transfer Analysis of a Tri-Dimensional Engine Internal Cavity, ICAS 2004-6.1.2 Propulsion
Design Procedure and Experimental Evaluation of Pressure-Swirl Atomizers, ICAS 2004-6.1.R.1 Propulsion
ENGINE STARTING PERFORMANCE EVALUATION AT STATIC STATE CONDITIONS USING SUPERSONIC AIR INTAKE, ICAS 2004-6.6.4 Propulsion
Flow-Field of a 12-Lobe Convoluted Mixer, ICAS 2004-6.5.2 Propulsion
Incidence Effects on the Aerodynamic Performance of the NEXST-2 Supersonic Intake Mounted Underneath a Wing, ICAS 2004-6.5.1 Propulsion
Increased RBCC Ejector Performance through Area Constriction, ICAS 2004-6.6.3 Propulsion
Integrated Aircraft Engine Design - The Implementation of the Master Model Concept at GE Aircraft Engines, ICAS 2004-6.4.2 Propulsion
Low-Emission Combustion Chamber Walls Cooling, ICAS 2004-6.1.1 Propulsion
Multi-Objective Optimization of Low Pressure Compression System, ICAS 2004-6.2.2 Propulsion
Numerical Simulation of the Spread of Rocket Plume, ICAS 2004-6.6.R Propulsion
Parametric Study of Liquid Rocket Engine System using Liquefied Natural Gas/Liquid Oxygen as Propellants, ICAS 2004-6.4.R Propulsion
PIV and Wall Convective Heat Transfer Measurements in a Round Jet in Cross-flow, ICAS 2004-6.1.3 Propulsion
PROGRESS IN DEVELOPING Innovative Flow Control in a Cascade Thrust Reverser, ICAS 2004-6.5.3 (St.) Propulsion
Research and Technology Development of Environmentally Compatible Propulsion System for Next Generation Supersonic Transport (ESPR Project) III. Final Achievements, ICAS 2004-6.4.4 Propulsion
Review of Propeller-Wing Aerodynamic Interference, ICAS 2004-6.3.1 Propulsion
Spray Characteristics of a Liquid-Liquid Coaxial Swirl Atomizer at Different Mass Flux Ratios, ICAS 2004-6.1.4 Propulsion
The Impact of Forward Sweep on Tip Clearance Flows in Transonic Compressors, ICAS 2004-6.2.1 Propulsion
Time Series Measurements of Mixing Condition of Hydrogen – Air Supersonic Mixing Layer, ICAS 2004-6.6.2 (St.) Propulsion
ULTRA AND VERY LIGHT DUCTED FAN PROPULSION SYSTEM COMPLEX DESIGN OPTIMIZATION, ICAS 2004-6.3.3 Propulsion
Use of Advanced CFD for the Design of Snecma Moteurs Turbomachine, ICAS 2004-6.4.3 Propulsion
Vortex Dynamics in Starting Square Water Jets, ICAS 2004-6.1 (St.).R.2 Propulsion
AIRCRAFT ENGINE ENVIRONMENTAL ISSUES AND ACTIVITY PLAN OF JAXA, ICAS 2004-7.10.1 Propulsion/ISABE
CFD Prediction of Unsteady Pressures due to Fan Rotor-Stator Interaction, ICAS 2004-7.10.2 Propulsion/ISABE
Current R&D Activities in National Aerospace Laboratory of Japan, ICAS 2004-6.7.5 Propulsion/ISABE
Dominant Parameter to Extinction Limit of Premixed Counterflow Flame under Various Pressures, ICAS 2004-6.8.1 Propulsion/ISABE
FLAME STABILIZATION AND NOX REDUCTION IN A NON-PREMIXED BURNER WITH SAWTOOTH MIXER, ICAS 2004-6.8.2 Propulsion/ISABE
Hypersonic Propulsion: The Future is Now, ICAS 2004-6.7.3 Propulsion/ISABE
Multi-Passage Gasdynamic Interactions in Wave Rotor, ICAS 2004-7.10.3 Propulsion/ISABE
NUMERICAL FLOW INVESTIGATION OF AN ANNULAR S-SHAPED DUCT, ICAS 2004-7.10.5 Propulsion/ISABE
Propulsion Vision for the 21st Century: Where We Are and Where We Are Going, ICAS 2004-6.7.1 Propulsion/ISABE
Rolls-Royce Propulsion Systems Technology – A Vision for the Future, ICAS 2004-6.7.2 Propulsion/ISABE
Scramjet Performance Achieved in Engine Tests from M4 to M8 Flight Conditions, ICAS 2004-6.8.3 Propulsion/ISABE
TBD, ICAS 2004-6.7.4 Propulsion/ISABE
Transient Performance Simulation of Propulsion System for CRW Type UAV Using SIMULINK ®, ICAS 2004-7.10.4 Propulsion/ISABE
Analysis of Human Pilot Manuever using Neural Network Modeling, ICAS 2004-7.11.1 Safety and Security
Application of Military and Aerospace RAMS Standards in Large Infra-Structure Projects – Railway Case Study, ICAS 2004-8.6.R Safety and Security
Application of Modified BP NN in Aircraft Engine Faults Diagnosis, ICAS 2004-8.8.3 (St.) Safety and Security
Concept for Hull-Loss Free Aircraft – Fuzzy Expert for More Advanced Automation in Flight Control, ICAS 2004-8.8.2 Safety and Security
Crashworthiness Shape Optimization of Helicopter Subfloor Intersection Elements, ICAS 2004-8.7.5 Safety and Security
Current Situation of Aviation Safety Information Exchange Systems in Japan, ICAS 2004-8.6.2 Safety and Security
Definition of an Optimal Damper For Helicopter Crashworthy, ICAS 2004-8.7.R.1 Safety and Security
DETECTION INDICES FOR A MINIATURISED HEALTH AND USAGE MONITORING SYSTEM UNIT, ICAS 2004-8.8.1 (St.) Safety and Security
Equivalent Corrosion Factors for Assessing Calendar Life of Aircraft Structures, ICAS 2004-8.8.R Safety and Security
Evaluation of Finite Element Modeling Methodologies for the Design of Crashworthy Composite Commercial Aircraft Fuselage, ICAS 2004-8.7.4 Safety and Security
Flight Demonstration of a New Operational Concept using TDMA Data Link System, ICAS 2004-7.11.R Safety and Security
High Energy Absorbing Composite Structure for Rotorcraft Crashworthiness, ICAS 2004-8.7.3 Safety and Security
Human-Centered Cockpit Study, ICAS 2004-7.11.3 Safety and Security
Hybrid Bayesian Method for reliability evaluation of aircraft structure, ICAS 2004-P.4 Safety and Security
Military Rotorcraft Qualification in the Netherlands - The Role Of NLR, ICAS 2004-8.6.3 Safety and Security
Multi-Objective Genetic Optimization of Helicopter Seats under Crashworthiness Requirements, ICAS 2004-8.7.2 Safety and Security
Structural Loading of a Complete Aircraft under Realistic Crash Conditions: Generation of a Load Database for Passenger Safety and Innovative Design, ICAS 2004-8.7.1 Safety and Security
Study of Landing Technique during Visual Approach, ICAS 2004-7.11.2 Safety and Security
TECHNOLOGICAL TRENDS IN SIMULATION TECHNOLOGY IN AVIATION & PILOT TRAINING, ICAS 2004-8.6.4 Safety and Security
Training Aspects of Implementation of JAR Regulations in the Czech Republic, ICAS 2004-8.6.1 Safety and Security
A VALUE PERSPECTIVE ON AEROSPACE INNOVATION, ICAS 2004-7.9.1 (I.L.) Systems Engineering and Supply Chain
Aircraft and Air Transportation Systems Curriculum at MIT, ICAS 2004-7.8.1 Systems Engineering and Supply Chain
An Approach to Improve Airframe Conceptual Design Process, ICAS 2004-7.7.2 Systems Engineering and Supply Chain
Automation of Manufacturing Cell using an Industrial Robot and Controlled by PLC, ICAS 2004-P.28 Systems Engineering and Supply Chain
Concurrent Engineering Development and Practices for Aircraft Design at Airbus, ICAS 2004-7.7.1 Systems Engineering and Supply Chain
Design for Customer, ICAS 2004-7.7.R.2 Systems Engineering and Supply Chain
Implementing Innovation in a Complex Context - The Aerospace Application, ICAS 2004-7.9.2 (I.L.) Systems Engineering and Supply Chain
Jobs Scheduling with Early-Tardy Penalties in Manufacturing Systems, ICAS 2004-P.31 Systems Engineering and Supply Chain
Manufacturing and Economic Constraints on the Structural Design of a Reduced-sized Technological Demonstrator, ICAS 2004-7.7.5 Systems Engineering and Supply Chain
Mechanical Model Centric Design in Lockheed Martin, ICAS 2004-7.7.3 Systems Engineering and Supply Chain
MULTI-PLATFORM INTEGRATED DEVELOPMENT AID SYSTEM (MIDAS), ICAS 2004-7.7.4 (St.) Systems Engineering and Supply Chain
THE DEVELOPMENT OF SCIENCE BASED PRODUCTS: MANAGING BY DESIGN SPACES, ICAS 2004-7.9.3 (I.L.) Systems Engineering and Supply Chain
The Development of the SYNAMEC a Design Tool for Aeronautical Mechanisms Applied to Leading Edge Devices, ICAS 2004-7.7.R.1 Systems Engineering and Supply Chain
An Overview of the De-Icing and Anti-icing Technologies with Prospects for the Future, ICAS 2004-7.5.1 (I.L.) Systems, Subsystems and Equipments
Avionics Systems Implementation - Benefits from Theoretical Computer Science, ICAS 2004-7.4.4 Systems, Subsystems and Equipments
Development of Ice Accretion and Anti-Icing System Simulation Code, ICAS 2004-7.5.R.2 Systems, Subsystems and Equipments
Fault Tolerant Flight Control Hydraulic System for Helicopters, ICAS 2004-7.6.4 Systems, Subsystems and Equipments
FENSAP-ICE: A Full-3D In-Flight Icing Simulation System for Aircraft, Rotorcraft and UAVs, ICAS 2004-7.5.3 Systems, Subsystems and Equipments
Flap Control Systems: Proposal of Advanced Asymmetry Monitoring Techniques, ICAS 2004-7.6.1 Systems, Subsystems and Equipments
From Test Rig to Innovative Modular FCS Test Environment, ICAS 2004-7.4.3 Systems, Subsystems and Equipments
Fuel Cell APU’s in Commercial Aircraft – an Assessment of SOFC and PEMFC Concepts, ICAS 2004-7.6.3 Systems, Subsystems and Equipments
Indian Advanced Light Helicopter Special Test Instrumentation, ICAS 2004-P.13 Systems, Subsystems and Equipments
INTEGRATED EQUIPMENT SYSTEMS FOR A MORE ELECTRIC AIRCRAFT – HYDRAULICS AND PNEUMATICS, ICAS 2004-7.4.2 Systems, Subsystems and Equipments
Intelligent System Transporter, ICAS 2004-P.29 Systems, Subsystems and Equipments
Modeling of a Three-Phase Application of a Magnetic Amplifier, ICAS 2004-7.6.2 Systems, Subsystems and Equipments
Multiple Stream PCM Data Handling System for Processing of Flight Test Data From Modern Prototype Helicopters, ICAS 2004-P.12 Systems, Subsystems and Equipments
Numerical Simulation of Airfoil Ice Accretion and Thermal Anti-Ici Systems, ICAS 2004-7.5.2 Systems, Subsystems and Equipments
Some Concepts on the Separable Landing System of Airplane, ICAS 2004-7.6.R.2 Systems, Subsystems and Equipments
SPECIFIC FEATURES OF HIGH PRESSURE WATER SEPARATION IN AIRCRAFT ENVIRONMENTAL CONTROL SYSTEMS, ICAS 2004-7.5.R.1 Systems, Subsystems and Equipments
TBD, ICAS 2004-7.6.R.1 Systems, Subsystems and Equipments
Technology Programs for Landing Gear Systems, ICAS 2004-7.4.5 Systems, Subsystems and Equipments
Tools and Methodology for Collaborative Systems Design Applied on More Electric Aircraft, ICAS 2004-7.4.1 Systems, Subsystems and Equipments
GARTEUR: 30 Years of European Collaboration in Aeronautics Research, ICAS 2004-0.6: VON KARMAN LECTURE: VON KARMAN LECTURE