Authors Index

Last Name
Initial
Paper Number Link to the Abstract Paper Title
ACAR H. 3.1.4 An Experimental Investigation of a Rectangular Jet Impinging on a Flat Surface Obliquely
ACCARDO A. F. 1.3.1 Design and Development of a Low Altitude Unmanned Aerial Vehicle
ACHAIBOU K. 1.9.3 Trajectory Generation and Display for Free Flight
AILER P. 7.5.2 Mathematical Modelling of a Low Power Gas Turbine Engine and Its Control System
ALLAIN C. 3.1.2 Flow Velocity Investigation by Embedded Laser Doppler Velocimetry on 3D Oscillating Wings
ALVAREZ GARCIA J. J. 6.3.3 Flow Control Electro-Hydraulic Servo Valve Assembly with in-Built Automatic Failure Detection and Compensation
AMATO M. 2.7.3 Nonlinear k-e Turbulence Modeling for Industrial Applications
AMOLI A. 5.5.R1   Two Dimensional Simulation of Nozzleless Solid Rocket Motor Internal Ballistics
ANCIK Z. 2.11.R1 The Effect of Ice-Accretion on the Lateral Controlability
ANDERSON B. 6.11.2 Active Inlet Flow Control Technology Demonstration
ANDERSSON S. 3.6.3   Unmanned Air Vehicles
ANDREI I. 5.1.R1   Contributions on Generalising the Air Breathing Propulsion Systems; the Multiple Jet Engine
ANGHILERI M. 4.11.R1   Multiple Impact of a Single Bird Against the Intake of a Turbofan Experimental and Numerical Activity
ARNAL D. 3.4.2 Effect of Sound on Laminar Turbulent Transition on Swept Wings
ARNDT R. 6.1.2 Insulation Concept & Material Optimisation in Business Aircraft
ASAI K. 3.3.3 Pressure Sensitive Paint Application at Large Production Wind Tunnels
ASHILL P. 2.10.5 CFD Study of Shock Control at Cranfield
ASO S. 2.10.R1 Improvement of Aerodynamic Characteristics of Next Generation SST Wing by Lateral Blowing
ASO S. 3.5.3 Experimental Study on Self Induced Excitation Phenomena of Opposing Jet in Supersonic Flow
ASTARITA T. 5.5.3 Heat Transfer in a 180Deg Turn Ribbed Square Channel
ATLI V. 3.1.4 An Experimental Investigation of a Rectangular Jet Impinging on a Flat Surface Obliquely
AUBRUN S. 3.4.2 Effect of Sound on Laminar Turbulent Transition on Swept Wings
AUPOIX B. 3.4.R1 On the Characteristics of Incompressible Turbulent Boundary Layers
AZEVEDO J. L.F. 2.3.3 Flow Simulation over a Complete Satellite Launcher with a Cluster Configuration
BALLMANN J. 4.8.3 Navier-Stokes Based Direct Numerical Aeroelastic Simulation
BANERJEE J.R. 4.7.3 Flutter Analysis of Composite Wings Using Symbolic Computation
BARANOV N. 5.6.2 Mathematical Modeling for Studying the Conditions of Air Ammunition Warfare
BARBERO S. 5.6.3   New Methodologies in the Integrated Approach to External Store Separation Problem Optimisation of Camera Positioning for Flight Test
BARDAGI T. 5.2.3   Particle Ingestion in Engines of Military Transport Aircraft
BARNES T. J. 4.3.3 The FFA Operational Loads Monitoring Program - Achievements and Problems
BARRERA L. 2.8.1 AeroStation - A COBRA Components Approach to Aerodynamic Design Framework
BASSO E. 2.3.3 Flow Simulation over a Complete Satellite Launcher with a Cluster Configuration
BASSO P. 1.3.1 Design and Development of a Low Altitude Unmanned Aerial Vehicle
BATTILOMO L. 4.3.4 Global Residual Damage Evaluation of Impacted Sandwich Panels at Low Energy
BAUMINGER S. 1.2.2 Development of a Cargo Aircraft, an Overview of the Preliminary Aerodynamic Design Phase
BELOTSERKOVSKI A. 5.6.2 Mathematical Modeling for Studying the Conditions of Air Ammunition Warfare
BEN-ASHER J. 4.9.3 Active Control of Flexible Structures Based on Fuzzy Logic
BERA J. 5.9.4 Mathematical Model Based Methods to Investigate Manufacturing Anomalies
BERGGREN M. 2.4.5 Accuracy of Gradient Computations for Aerodynamic Shape Optimisation Problems
BERGLJUNG P. 1.11.1   NINS/NILS - A New Navigation and Landing System for JAS39 Gripen
BERGSTROM M. 3.11.3 The Use of Desktop Simulations in the Carefree Maneuvering Flight Test Program of JAS39 Gripen
BERNAY B. 5.3.2 Aircraft Engine Response Due to Fan Unbalance and to the Presence of "Consumed" Gaps in the Engine during The Phase of Windmilling
BERRY P. 1.7.2 Integration of Subscale Flight Testing Design Education
BERTON E. 3.1.2 Flow Velocity Investigation by Embedded Laser Doppler Velocimetry on 3D Oscillating Wings
BETZ D. 4.9.R1 Fiberoptic Smart Sensing of Component Deformations in Adaptive Wings
BEYERS M. E. 3.10.3 Requirements for Subscale Simulation of Delta-Wing Vortex Characteristics
BICKARD T. 6.2.1 Maintenance Optimisation of a Digital Engine Control System with Limit Failure Rate Constrain
BIENCZAK K. 6.8.3   A Stochastic Model of Friction Effected Degradation of Airborne Tribological Systems, as Used to Solve Diagnostic Problems
BIL C. 1.3.2 Design of Optimum Payloads to Meet the Mission Requirements of UAV Systems
BIL C. 3.6.4 Dynamic Control Aspects of the Shipboard Launch of Unmanned Air Vehicles
BINKS D. 6.8.1 The Numerical Simulation and Experimental Validation of Ventilation Flow and Fire Events in a Trent Nacelle Fire Zone
BIRCH N. 1.1.1 (IL) 2020 Vision : Prospects for Large Civil Aircraft Propulsion
BIRCH T. J. 2.4.2 Towards an Efficient Robust and Accurate Numerical Solver for Supersonic Viscous Flows
BIRON D. 3.4.2 Effect of Sound on Laminar Turbulent Transition on Swept Wings
BIRRENBACH R. 1.2.1 (IL) 728 : A New Family of Regional Transports Aircraft
BISAGNI C. 4.1.4   Compression and Torsion Buckling Tests on Fiber Composite Cylinders
BLOBNER F. 6.4.1 (IL)   Human Centered Design Flight Deck Design and Utility System Integration
BLOM H. A.P. 6.5.2 Assessment of Wake Vortex Safety to Determine Adequately Safe Separation Distances
BODAGHABADI S. 2.3.4 Three Dimensional Unstructured Grid Generation for Finite Volume Solution of Euler Equations
BOGOS S. 2.1.4 The Aerodynamic and Dynamic Ventral Fins Effects on a Jet Trainer
BOLSUNOVSKY A.L. 1.1.R2 Investigations on Possible Characteristics of FW Superhigh Seating Capacity Airplane
BORELLO L. 1.7.4 An Academic Experience on Aircraft Design : Affordable Advanced Jet Trainer
BOURBAN C.M. 6.1.2 Insulation Concept & Material Optimisation in Business Aircraft
BOUSSEMART M. 6.2.1 Maintenance Optimisation of a Digital Engine Control System with Limit Failure Rate Constrain
BOYER M. 3.9.2 Airport Noise / Annoyance Analysis
BRÄMER E. 1.9.1 ASAS - Investigations Into Airborne Separation Assurance in a Distributed Simulation Environment
BREITSAMTER C. 3.10.2 Fin Buffet Load Alleviation Using an Actively Controlled Auxiliary Rudder at Sideslip
BRITTEN G. 4.8.3 Navier-Stokes Based Direct Numerical Aeroelastic Simulation
BRODIE I. 6.2.2 Qualifications Chasing Avionics Technology?
BROICHHAUSEN K. 3.8.3   The European Initiative Towards Ultra Low Emission Engines
BRUNDLE D. 5.4.4   A Cost-Based Analysis of UK Guided Bomb Solutions and Issues Associated with the Integration of COTS Components
BRUUN H.H. 2.9.R2 Experimental Investigation of Flowfield over a Multi-element Aerofoil and Comparison with Computational Prediction
BURLEY G. 5.9.2 Error Budgeting and the Design of Large Aerostructures
BUTLER R. 4.7.3 Flutter Analysis of Composite Wings Using Symbolic Computation
BUZOVERYA N.P. 1.1.R2 Investigations on Possible Characteristics of FW Superhigh Seating Capacity Airplane
CAMATTI D. 7.4.5 Digital Mock-up : A Useful Tool in Aircraft Design
CAMPOS L.M.B.C. 1.10.2   On the Wake Vortex Hazard and Aircraft Safe Separation
CAMPOS L.M.B.C. 3.9.R2   Comparison of Prediction and Measurements on Propeller Noise at an Angle of Attack
CARDONE G. 5.5.3 Heat Transfer in a 180Deg Turn Ribbed Square Channel
CARLOMAGNO G.M. 5.5.3 Heat Transfer in a 180Deg Turn Ribbed Square Channel
CASTELLETTI L. 4.11.R1   Multiple Impact of a Single Bird Against the Intake of a Turbofan Experimental and Numerical Activity
CASTIES C. 2.8.1 AeroStation - A COBRA Components Approach to Aerodynamic Design Framework
CATALANO F. M. 3.4.4 On the Effects of a Installed Propeller Slipstream on a Wing Boundary Layer
CATALANO F. M. 7.4.3 Conceptual Design and Optimization of a High Aspect Ratio UAV Wing Made of Composite Material
CATALANO F. Martini 7.7.1 An Experimental Study on Wingtip Devices for Agricultural Aircraft
CATALANO P. 2.7.3 Nonlinear k-e Turbulence Modeling for Industrial Applications
CEBECI T. 2.2.2 An Engineering Approach to the Calculation of Two and Three Dimensional Flows with Extensive Separation
CEBECI T. 2.7.5 Prediction of Aeroelastic Effects of Aircraft Configurations Including High Lift Systems
CENKO A. 5.6.1 A CFD Applications to Store Sparation - Status Report
CERVIA A. B. 5.7.4 Optimisation of the Aircraft Development Process in Small Aircraft Companies
CHANG K.C. 2.7.5 Prediction of Aeroelastic Effects of Aircraft Configurations Including High Lift Systems
CHANG K.C. 2.2.2 An Engineering Approach to the Calculation of Two and Three Dimensional Flows with Extensive Separation
CHAPUT E. 2.8.1 AeroStation - A COBRA Components Approach to Aerodynamic Design Framework
CHARLES J.L. 4.11.3 Improvement of Crash Models of Large Aeronautical Structures
CHARLTON E. 4.8.1 Computational Aeroelasticity in High Performance Aircraft Flight Loads
CHAUDRON L. 3.9.2 Airport Noise / Annoyance Analysis
CHAUDRON L. 6.7.2 REX : a Human Factor Flight Safety Research Program
CHAUVEAU J. P. 7.6.1 Use of Navigation Satellite Systems for Aircraft Operations : Sensitivity to Errors
CHEN C. 6.5.R1 Flying Quality Study under the Influence of Clear Air Turbulence
CHEN H.H. 2.7.5 Prediction of Aeroelastic Effects of Aircraft Configurations Including High Lift Systems
CHEN H.H. 2.2.2 An Engineering Approach to the Calculation of Two and Three Dimensional Flows with Extensive Separation
CHEN R. 4.9.R2 Development and Testing of an Adaptive Rotor System Based on Solid Actuation and Non Contact Signal Transmission Technology
CHEN Y. 4.9.R2 Development and Testing of an Adaptive Rotor System Based on Solid Actuation and Non Contact Signal Transmission Technology
CHERN J. 1.10.5   Intensity and Time Considerations in Microburst Penetration
CHESTER D. Harold 4.11.2 A Parametric Study of Aircraft Landing-Impact with Emphasis on Nose-Gear Landing Design Conditions
CHEVALIER M. 2.4.5 Accuracy of Gradient Computations for Aerodynamic Shape Optimisation Problems
CHIESA S. G. 1.7.4 An Academic Experience on Aircraft Design : Affordable Advanced Jet Trainer
CHOU H. S.Y. 3.2.2 Aerodynamic Design and Analysis of a Reusable Launch Vehicle
CHRISTOPHE B. P. 7.6.1 Use of Navigation Satellite Systems for Aircraft Operations : Sensitivity to Errors
CHUGG A. 6.4.4 Cosmic Radiation Effects Upon Avionics - An Increasing Hazard in the New Millennium ?
CLARK G. 4.4.4 The Significance of Laminar Corrosion Defects in Aircraft
COENEN E. 7.3.1 Quasi-Simultaneous Viscous Inviscid Interaction for Three Dimensional Turbulent Wing Flow
COHEN K. 4.9.3 Active Control of Flexible Structures Based on Fuzzy Logic
COIMBRA R. F.F. 7.7.1 An Experimental Study on Wingtip Devices for Agricultural Aircraft
COLDBECK D. 1.7.1 Changing Education Requirements for Design Engineers
COLLERCANDY R. 2.6.1 Navier-Stokes Calculations at Aerospatiale-Airbus for Aircraft Design
COLWELL B. 6.4.4 Cosmic Radiation Effects Upon Avionics - An Increasing Hazard in the New Millennium ?
CONEY M. H. 6.8.1 The Numerical Simulation and Experimental Validation of Ventilation Flow and Fire Events in a Trent Nacelle Fire Zone
CONWAY J.T. 2.1.1 Numerical Analysis of the Aerodynamics of the Aurora Aircraft by an Inviscid / Viscous Interaction Method
COOPER C. 5.9.1 (IL) Agile Manufacturing Processes
COOPER J.E. 4.6.4 Prediction of Non-Linear Aeroelastic Instabilities
COOPER K.R. 3.7.5 Wind Tunnel Wall Constraint: Extension to Three Dimensions
COOPER R. 2.3.R1 Simulation of 3-Dimensional Incompressible Cavity Flows
CORBETT J. 5.9.2 Error Budgeting and the Design of Large Aerostructures
CORPINO S. 7.4.5 Digital Mock-up : A Useful Tool in Aircraft Design
COX T.H. 4.10.4 Path-Attitude Inconsonance in High Speed Flight and Related Path Control Issues
CREPIN P.Y. 6.3.1 Model Based Fault Detection for an Aircraft Actuator
CROOK A. 2.10.3 The Interaction of a Synthetic Jet with a Turbulent Boundary Layer
CROSS M.R. 2.7.2 Aerodynamic Design Using the Euler Adjoint Approach
CROZIER M. 5.4.5   Hovering Off-Board Decoy Development Programme and Technologies
CRUMP M. R. 3.6.4 Dynamic Control Aspects of the Shipboard Launch of Unmanned Air Vehicles
CZERWIEC R. M. 3.4.5 Transition Onset Predictions for High-Lift Configurations
DAFNIS A. 4.6.2 Design and Qualification Concepts for Flexible Wind Tunnel Wing Models
DAMILANO J. G. 4.6.R1 Nonlinear Elastic Constrained Multibody Systems - An Adaptive Time-Stepping Algorithm Based on the Time-Discontinuous Galerkin Scheme
DAMODARAN M. 2.11.2 Airfoil Design Optimisation using Navier-Stokes Equations and Simulated Annealing
DEASLEY P.J. 5.7.3 A Distributed Design Scenario for Aerospace
DEGAKI T 7.2.1 Active Flutter Suppression for Nonlinear Aeroelastic System
DELAGARZA A. 4.8.1 Computational Aeroelasticity in High Performance Aircraft Flight Loads
DELAURENTIS D. 1.4.4 Methodology for Examining the Simultaneous Impact of Requirements, Vehicle Characteristics, and Technologies on Military Aircraft Design
DEMATTEIS P. 2.10.R2   A New Concept for the Adaptive Shock and Boundary Layer Control on Transonic Flows about Airfoils
DEMENTYEV A.D. 4.4.1 Problems of Ensuring Structural Life of the Second Generation Supersonic Transport
DENISOV V. E. 1.1.R2 Investigations on Possible Characteristics of FW Superhigh Seating Capacity Airplane
DERISHEV S. G. 1.2.3 Propeller Airframe Aerodynamic Interference on Twin Engine Aircraft
DEVIES G.A.O. 4.1.2 Modelling of Damage in Fibre Reinforced Composite Laminates under Multiaxial In-plane Loading
DEVRIES T.J. 4.5.R2 Towards Technology Readiness of Fibre Metal Laminates
DEY D. 6.4.3 The Development of a Civilian Fly by Wire Flight Control System
DICICCA G.M. 2.10.2 Flow Control Downstream of a Backward Facing Step
DICICCA G.M. 7.3.3 PIV Study of Longitudinal Vortices in a Turbulent Boundary Layer Flow
DIMA C. 2.10.R2   A New Concept for the Adaptive Shock and Boundary Layer Control on Transonic Flows about Airfoils
DIRKS G. 5.10.3 Scenario Based Aircraft Design Using Knowledge Based Software Methods
DIXON R. 5.11.1 Systems Engineering in Marketing & Economics of Aero Engines
DJOJODIHARDJO H. 4.7.2 Optimization of Tapered Wing Structures With Aeroelastic Constraints
DORIGNAC E. 5.5.1 Temperature and Convective Heat Transfer Coefficient Profiles Downstream a Multiperforated Plate - Application to Combustion Chamber Cooling
DORRINGTON G.E. 1.7.5 University Development of A Derivative Aircraft Based on A Kit-Glider
DOUKAS L. 5.11.1 Systems Engineering in Marketing & Economics of Aero Engines
DYER C. 6.4.4 Cosmic Radiation Effects Upon Avionics - An Increasing Hazard in the New Millennium ?
DZYGADLO Z. 1.8.3 Nonlinear Dynamic Model for Flexural Vibrations Analysis of a Supercritical Helicopter's Tail Rotor Drive Shaft
DZYGADLO Z. 2.7.R1 Numerical Structural Analysis of Viscous Compressible Flow Past an Airfoil and Body of Revolution
EARLY K. 6.10.3 Propulsion-Airframe Integration Design, Analysis and Challenges going into the 21st Century
EAST R.A. 5.4.2 Hypersonic Missiles - Some Aerothermodynamic Problem Area
EASTEP F.E. 1.4.1 Flexible Composite Wing with Internal Actuation for Roll Maneuver
EBERLE A. 4.8.2 Coupled Steady and Unsteady Aeroelastic Simulations in the Transonic Flight Regime
EDWARDS J.A. 3.5.2 Computation of a Dynamically Deployed Flap Employing Adaptive Body Recovery
EDWARDS J.A. 5.4.2 Hypersonic Missiles - Some Aerothermodynamic Problem Area
EDWARDS J.R. 3.4.5 Transition Onset Predictions for High-Lift Configurations
EDWARDS R. 5.11.R1   A Method for the Assessment of Technology Transparency
EGLE D. 4.8.1 Computational Aeroelasticity in High Performance Aircraft Flight Loads
EISENLOHR   1.11.2   Training of Military Pilots
ERHARD W. 5.1.4 Advances in Turboengine Real-Time Simulation for Modern Control System Development
ERICSSON L. E. 3.10.3 Requirements for Subscale Simulation of Delta-Wing Vortex Characteristics
ERIM M.Z. 7.7.4   On the Calibration of 30x60 mm Trisonic Wind Tunnel at the Istanbul Technical University
ESHELBY M. 1.10.4 Design and Validation Using Flight Data of a Method for Predicting the Ground Run Required for Take-off
EUSTACE P. 1.6.3 Predicting the Effects of New Technologies on Aircraft Structural Mass : UCAV Case Study
EVANS L. 5.11.3 Shaping The Successful Implementation of Human Factors Integration
EVANS M.C.W. 3.7.3 Ground Effect Testing Capabilities in the Filton 12' x 10' Low Speed Wind Tunnel
EVANS S. 5.7.3 A Distributed Design Scenario for Aerospace
EYI S. 5.1.3 Inverse Design of Turbomachinery Airfoils Using the Navier Stokes Equations
FAN J. 4.4.5 Calendar Fatigue Life of Airframe Materials
FARES E. 2.1.2 Numerical Simulation of he Interaction of Side Flap Vortices and Engines Jets
FAVIER D. 3.1.2 Flow Velocity Investigation by Embedded Laser Doppler Velocimetry on 3D Oscillating Wings
FEY I. 6.4.5 Model Based Software Development and Code Generation for Avionic Systems
FIELDING C. 3.11.1 Stability and Control of STOVL Aircraft
FIELDING J. P. 5.7.3 A Distributed Design Scenario for Aerospace
FIELDING J.P. 1.2.R1 Design Investigation of Variable Camber Flaps for High-Subsonic Airliners
FIELDING J.P. 1.6.2 Design Synthesis and Optimisation of an Advanced Short Take -off and Vertical Landing (ASTOVL) Combat Aircraft
FIFKA P. 2.11.R1 The Effect of Ice-Accretion on the Lateral Controlability
FILATYEV A.S 4.10.5 New Solutions of the Optimal Injection Problems Based on Complex Investigation of Dynamics and Aerodynamics
FISCHER M. 4.2.3 Local Postbuckling Analysis of Curved Aerospace Structures
FRAGIAS A. P. 3.9.4 Influence of Arbitrary Vortical Wake Evolution on Flowfield and Noise Generation of Helicopter Rotors
FRICKE H. 1.9.1 ASAS - Investigations Into Airborne Separation Assurance in a Distributed Simulation Environment
FRINK N. T. 2.4.1 (IL) The NASA Tetrahedral Unstructured Software System
FUCHS L. 5.2.2 Vortex System and the Interference Between an Air Intake and the Ground
FUIOREA I. 4.11.R2 A Point of View Regarding to Dynamic Analysis of an Aircraft Structure
FUJIMORI A. 4.10.R2 Model Modification of Transonic Aerodynamic Force on a High-Aspect Ratio Aeroelastic Wing and its Active Flutter
G.SLAMA J. 1.9.3 Trajectory Generation and Display for Free Flight
GACHERIEU C. 2.6.1 Navier-Stokes Calculations at Aerospatiale-Airbus for Aircraft Design
GAERKE J. 4.5.R1 Predicting Fatigue Life Improvement In Cold Expanded Fastener Joints
GALPIN S.A. 2.7.1 The Application of a Time Accurate Unstructured Euler Solver Coupled with a Boundary Layer Solver for the Solution of Transonic Aeroelastic Problems on Complex Configurations
GAO W. 4.9.R2 Development and Testing of an Adaptive Rotor System Based on Solid Actuation and Non Contact Signal Transmission Technology
GAO Z. 7.4.2 Aerodynamic Configuration Design of Aircraft Using Multi-objective Genetic Algorithm
GAUSZ T. 1.8.2 Aerodynamical and Dynamical Investigation of Helicopter Rotors
GAUTREY J 6.9.R1 Flying Qualities Design for a Fly-by-Wire Transport Aircraft in the Landing Flight Phase
GEMMA R. 5.6.3   New Methodologies in the Integrated Approach to External Store Separation Problem Optimisation of Camera Positioning for Flight Test
GERLE M. 4.9.4 Actuator Technology Based on Smart Materials for Adaptive Systems in Aerospace
GIAVOTTO V. 4.3.1 (IL)   Structural Optimization in Crashworthy Design
GIESBERTS M. 6.6.3 Precipitation Drag of Snow and Standing Water
GIRODO D. 5.6.3   New Methodologies in the Integrated Approach to External Store Separation Problem Optimisation of Camera Positioning for Flight Test
GIVOLI D. 4.2.R1 An Adaptative Finite Element Framework for Fatigue Crack Propagation
GOLIKOV A.A. 4.10.5 New Solutions of the Problem of Optimal Injection Trajectories Based on Complex Investigation of Dynamics and Aerodynamics
GOMAN M.G. 2.2.3 The Characteristic Time Constant Approach for Mathematical Modelling of High Angle of Attack Aerodynamics
GOODEN J. 6.6.3 Precipitation Drag of Snow and Standing Water
GORAJ Z. 3.6.2 Dynamics of High Altitude Long Endurance UAV
GORAJ Z. 4.7.R1 Ultra Light Wing Structure for High Altitude Long Endurance UAV
GOTO N. 6.9.4 Neal-Smith Criteria-Based Hoo Approach to Predicting Aircraft Handling Qualities
GRASHOF J. 4.8.2 Coupled Steady and Unsteady Aeroelastic Simulations in the Transonic Flight Regime
GRAU J.Y. 6.7.2 REX : a Human Factor Flight Safety Research Program
GREENWELL D. 1.6.1 Wing Design of an Oblique Wing Combat Aircraft
GREENWELL D. 2.2.3 The Characteristic Time Constant Approach for Mathematical Modelling of High Angle of Attack Aerodynamics
GU Z. 4.9.R2 Development and Testing of an Adaptive Rotor System Based on Solid Actuation and Non Contact Signal Transmission Technology
GUENOV M.D. 5.7.3 A Distributed Design Scenario for Aerospace
GUNAWAN L. 4.11.1 Experimental Study of Nonlinear Vibrations of Thin-Walled Cylindrical Shells
GUREVICH B.I. 1.1.R2 Investigations on Possible Characteristics of FW Superhigh Seating Capacity Airplane
GÜVEN A. 7.2.2 The Design of a System by which some of the Air Parameters are Transmitted Between Air and the Ground Station using a Model Aircraft
HAASE W. 4.8.2 Coupled Steady and Unsteady Aeroelastic Simulations in the Transonic Flight Regime
HACKETT J.E. 3.7.5 Drag, Lift and Pitching Moment Increments due to the Wind Tunnel Wall Constraint : Extension to Three Dimensions
HALL C. 6.11.3   F/A - 18 E/F - F414-GE-400 Propulsion System Integration
HAMSTRA J.W. 6.11.2 Active Inlet Flow Control Technology Demonstration
HANFF E.S. 2.2.1 Airload Predictions for Delta Wings at High Incidence
HANFF E.S. 3.10.1 Application of Dynamic Manipulation on the Forebody Vortices of a Schematic Aircraft Model
HARJANTO I. 4.7.2 Optimization of Tapered Wing Structures With Aeroelastic Constraints
HARMER S. 5.11.3 Shaping The Successful Implementation of Human Factors Integration
HASSAN H.A. 3.4.5 Transition Onset Predictions for High-Lift Configurations
HAUF T. 1.10.3 Airborne Observation of Ice Accretion and Aircraft Performance In Artificial and Natural Supercooled Ice Clouds on Dornier 228 and 328 Aircraft
HEINZE W. 1.4.5 Influence of Aeroelastic Effects on Preliminary Aircraft Design
HENKNER J. 2.9.2 Phenomena of Dynamic Stall on Swept Wings
HERMLE F. 4.9.4 Actuator Technology Based on Smart Materials for Adaptive Systems in Aerospace
HERMLE P. 6.4.2 Electronic Flight Display Development Supported by Commercial of the Shelf Tools
HILL R. 3.6.4 Dynamic Control Aspects of the Shipboard Launch of Unmanned Air Vehicles
HILLENHERMS C. 3.1.3 Transonic Flow Experiments with a 2-D Rectangular Wing Section Oscillating in Pitch
HOBZA P. 3.3.2 New Generation Portable Data Acquisition System
HOBZA P. 4.2.1 Optimum Design of A Stiffened Panel Using the Method of Mathematical Programming
HOEIJMAKERS H.W.M. 3.10.5   A Numerical Method to Simulate the Onset of Breakdown of an Unconfined Isolated Vortex Core
HOEIJMAKERS H.W.M. 6.5.3 Wake Vortex Simulations Using A Parallel High-Order Accurate Navier-Stokes Solver
HOFFMAN E. 1.9.2 Delegation of Separation Assurance to Aircraft : Towards a Framework for Analysing the Different Concepts and Underlying Principles
HOFFMANN M. 6.4.5 Model Based Software Development and Code Generation for Avionic Systems
HOLL M. 3.1.1 Wind Tunnel Testing of Performance Degradation of Ice Contaminated Airfoils
HOLMBERG G. 5.7.2 Integrated Product Development - a Key to Affordability
HOLROYD J. 6.7.1   Human Factors in Military Aircraft Accidents
HONDA K. 6.7.3 Workload Measurements for Operations under Simulated Single Pilot Instrument Flight Rules
HORROCKS D. M. 6.8.1 The Numerical Simulation and Experimental Validation of Ventilation Flow and Fire Events in a Trent Nacelle Fire Zone
HORST P. 1.4.5 Influence of Aeroelastic Effects on Preliminary Aircraft Design
HOSHIZAKI T. 6.9.4 Neal-Smith Criteria-Based Hoo Approach to Predicting Aircraft Handling Qualities
HSIAO F. 7.6.3 The Development of a Low Cost Navigation System Using GPS/RDS Technology
HU Z.Q. 4.5.3 Deformation Inhomogeneity in a Single Crystal Nickel Base Superalloy
HUANG X.Z. 2.2.1 Airload Predictions for Delta Wings at High Incidence
HUCHARD J. 2.8.1 AeroStation - A COBRA Components Approach to Aerodynamic Design Framework
HUETTIG G. 1.9.1 ASAS - Investigations Into Airborne Separation Assurance in a Distributed Simulation Environment
HUMAN M. 4.10.3 Minimum Emission Ascent and Descent Trajectories
HUMBERT M. 4.10.2 Identification of the Aeroelastic Model of a Large Transport Aircraft for Control Law Design and Validation
HUMMEL D. 2.5.2 Numerical Analysis of the Unsteady Flow Above a Slender Delta Wing at Large Angles of Attack
HUNG H. 1.3.R1 The Development of a Jet-UAV Conceptual Design Code
HUREZ A.J. 2.8.3 Recent Progress on Powerplant / Airframe Integration at AEROSPATIALE-AIRBUS
HUYTON P. 7.4.R1 Buckling of Skew Plates with Continuity or Rotational Edge Restraint
IGNATIEVA A. V. 2.1.R1 Optimization of a Given Planform Lifting System at Supersonic Speed
IKAZA D. 5.3.R1 Thrust Vectoring Nozzle for Military Aircraft Engines
IKRYANOV I. 7.5.3 The Influence of Stealth Technology on Flight Performance and Maneuvering Characteristics of Fighter Aircraft
IRELAND P. T. 6.8.2 Validation of Novel Low Temperature Fire Event Modelling Technique
ISHIDE T. 2.9.3 Experimental Investigation of Three Dimensional Separated Flow over a Body of Revolution at High Angles of Attack
ISHIKAWA H. 2.1.3 Supersonic Inverse Design of Wings for the Full Configuration of Japanese SST
ISHMURATOV F.Z. 4.6.3 Static Aeroelasticity Analysis in Transonic Flow
ISOGAI K. 4.7.5 Shock Stall Flutter a Two-Dimensional Airfoil
IWAMIYA T. 2.1.3 Supersonic Inverse Design of Wings for the Full Configuration of Japanese SST
JACKSON M. 5.9.1 (IL) Agile Manufacturing Processes
JAHANGIRIAN A.R. 2.3.2 A Solution Adaptive Grid Method for Calculation of High Speed Flows around Blunt Body Configurations
JÄNKER P. 4.9.4 Actuator Technology Based on Smart Materials for Adaptive Systems in Aerospace
JEBACEK I. 3.3.2 New Generation Portable Data Acquisition System
JENKINSON L. 1.6.3 Predicting the Effects of New Technologies on Aircraft Structural Mass : UCAV Case Study
JIN J. 5.3.4 Experimental Investigation of Static Internal Performance for an Axisymmetric Vectoring Thrust Nozzle (AVEN)
JIN J. 4.9.1 Theoretical and Experimental Study on Shape Memory Alloy Torsion Actuator
JIN T.J. 4.5.3 Deformation Inhomogeneity in a Single Crystal Nickel Base Superalloy
JING H. 6.7.4 On the Correlation between Cultural Background and the Commercial Aircraft Accidents
JOHANSSON K. 6.4.4 Cosmic Radiation Effects Upon Avionics - An Increasing Hazard in the New Millennium ?
JOHNSON F. 2.2.2 An Engineering Approach to the Calculation of Two and Three Dimensional Flows with Extensive Separation
JOHNSON J. 5.10.4 The Latest Developments in Design Data Exchange : Towards Fully Integrated Aerospace Design Environments
JONES R. 6.4.4 Cosmic Radiation Effects Upon Avionics - An Increasing Hazard in the New Millennium ?
JOUBERT H. 6.10.4 Turbomachinery Design Used Intensive CFD
JUNG W. 4.6.2 Design and Qualification Concepts for Flexible Wind Tunnel Wing Models
KADAR M. 2.5.3 Prediction of Aerodynamic - Lift Redistribution on Flexible Wing Structure Using Transonic Unsteady Aerodynamic Code - Ntrans
KAEMPF P. 1.5.1   High Altitude Long Endurance Aircraft
KALETTA P. 4.1.1 Optimization of Composite Aircraft Panels Using Evolutionary Computation Methods
KAMISHITA M. 2.10.R1 Improvement of Aerodynamic Characteristics of Next Generation SST Wing by Lateral Blowing
KÄMPCHEN M. 4.6.2 Design and Qualification Concepts for Flexible Wind Tunnel Wing Models
KANDA A. 6.6.2 Scattering Analysis for Wreckage of In-Flight Breakup
KANEVSKI M. 5.6.2 Mathematical Modeling for Studying the Conditions of Air Ammunition Warfare
KANIA W. 1.8.R1 Development of New Generation Main and Tail Rotors Blade Airfoils
KAPLAN A. 7.2.3 Target Tracking with the Use of Neural Networks
KAPLAN B. 5.1.3 Inverse Design of Turbomachinery Airfoils Using the Navier Stokes Equations
KARA S 7.2.2 The Design of a System by which some of the Air Parameters are Transmitted Between Air and the Ground Station using a Model Aircraft
KARASHIMA K. 2.10.R1 Improvement of Aerodynamic Characteristics of Next Generation SST Wing by Lateral Blowing
KARASHIMA K. 3.5.3 Experimental Study on Self Induced Excitation Phenomena of Opposing Jet in Supersonic Flow
KARIMIAN S.M.H. 5.5.R1   Two Dimensional Simulation of Nozzleless Solid Rocket Motor Internal Ballistics
KARLSSON A. 5.2.2 Vortex System and the Interference Between an Air Intake and the Ground
KASHTALYAN M. 4.1.2 Modelling of Damage in Fibre Reinforced Composite Laminates under Multiaxial In-plane Loading
KEHAYAS N. 1.6.2 Design Synthesis and Optimisation of an Advanced Short Take -off and Vertical Landing (ASTOVL) Combat Aircraft
KENNEDY D. 4.2.3 Local Postbuckling Analysis of Curved Aerospace Structures
KHALID M. 3.7.R2 The Art and Science of Wind Tunnel Wall Interference : New Challenges
KHOT N.S. 1.4.1 Flexible Composite Wing with Internal Actuation for Roll Maneuver
KHRABROV A.N. 2.2.3 The Characteristic Time Constant Approach for Mathematical Modelling of High Angle of Attack Aerodynamics
KIND R.J. 3.10.1 Application of Dynamic Manipulation on the Forebody Vortices of a Schematic Aircraft Model
KLEEMANN E. 6.4.3 The Development of a Civilian Fly by Wire Flight Control System
KLOMPE A.W.H. 4.11.1 Experimental Study of Nonlinear Vibrations of Thin-Walled Cylindrical Shells
KNOWLES K. 2.9.1 Comparison of Jet Induced Lift Loss for Single and Coaxial Jets
KOMATSU N. 3.3.3 Pressure Sensitive Paint Application at Large Production Wind Tunnels
KOPP S. 5.1.4 Advances in Turboengine Real-Time Simulation for Modern Control System Development
KOS J. 6.5.2 Assessment of Wake Vortex Safety to Determine Adequately Safe Separation Distances
KOSSIRA H. 4.5.1 Mixed Mode Fracture Characterization of Adhesive Joints
KOUZMINA S.I. 4.6.3 Static Aeroelasticity Analysis in Transonic Flow
KOUZNETSOV V. M. 3.9.R1 Efficiency of Ejector Devices and of Sound Absorbing Structures for Jet Noise Reduction
KRAVCHENKO S. 5.10.5   The Boeing Technical Research Center in Moscow - An Example of International Technology Development
KREINER A. 5.1.4 Advances in Turboengine Real-Time Simulation for Modern Control System Development
KRESS R. 6.3.1 Model Based Fault Detection for an Aircraft Actuator
KRUMPHOLZ O. 4.9.R1 Fiberoptic Smart Sensing of Component Deformations in Adaptive Wings
KRUS P. 1.7.2 Integration of Subscale Flight Testing Design Education
KRUS P. 6.1.3 Complete Aircraft System Simulation for Aircraft Design - Paradigms for Modelling of Complex System
KUNTJORO W. 5.3.3 In-Flight Thrust Determination by Load Measurement on the Engine Mounting System
KUSTRON K. 7.6.2   Model of Degradation of Metal Polimeric Composite Joints in Aspect of Reliability and Safety
LACABANNE M. 4.10.2 Identification of the Aeroelastic Model of a Large Transport Aircraft for Control Law Design and Validation
LACABANNE M. 4.7.1 (IL) Progress in the Prediction and Analysis of Aeroservoelastic Instabilities on Large Civil Transport Aircraft
LACROIX J. 7.6.1 Use of Navigation Satellite Systems for Aircraft Operations : Sensitivity to Errors
LAI C. 5.3.4 Experimental Investigation of Static Internal Performance for an Axisymmetric Vectoring Thrust Nozzle (AVEN)
LANCIOTTI A. 4.4.3 Durability Damage Tolerance and Environmentally Assisted Crack Propagation Characteristics of a Tig Welded Titanium Alloy
LANGRAND B. 4.11.3 Improvement of Crash Models of Large Aeronautical Structures
LAPORTE A. 4.7.1 (IL) Progress in the Prediction and Analysis of Aeroservoelastic Instabilities on Large Civil Transport Aircraft
LARRIEU P. 2.6.1 Navier-Stokes Calculations at Aerospatiale-Airbus for Aircraft Design
LASCHKA B. 3.10.2 Fin Buffet Load Alleviation Using an Actively Controlled Auxiliary Rudder at Sideslip
LAU F.J.P. 3.9.R2   Comparison of Prediction and Measurements on Propeller Noise at an Angle of Attack
LAZZERI L. 4.4.3 Durability Damage Tolerance and Environmentally Assisted Crack Propagation Characteristics of a Tig Welded Titanium Alloy
LEBLAYE P. 6.7.2 REX : a Human Factor Flight Safety Research Program
LEE B. P. 6.9.1 (IL) Recent Experience in Flight Testing for Pilot Induced Oscillations (PIO) on Transport Aircraft
LEE J. J. 3.8.2 Sustainable Aviation
LEE R. 3.10.1 Application of Dynamic Manipulation on the Forebody Vortices of a Schematic Aircraft Model
LEE S.L. 2.11.2 Airfoil Design Optimisation using Navier-Stokes Equations and Simulated Annealing
LEGARREC C. 4.10.2 Identification of the Aeroelastic Model of a Large Transport Aircraft for Control Law Design and Validation
LEHMANN O. 1.9.1 ASAS - Investigations Into Airborne Separation Assurance in a Distributed Simulation Environment
LEMOINE M. 1.10.1 An Information System for the Airport
LERUSALIMSKY K.M. 4.2.2 Stability of Built-up Cylindrical Structures with Consideration of Plastic and Postbuckling Behavior of Thin Walled Components
LESCHZINER M.A. 2.6.2 Numerical Investigation of Three-Dimensional Transonic Flow with Large Separation
LEUNG A.Y.T. 4.6.4 Prediction of Non-Linear Aeroelastic Instabilities
LEVIN M. 1.2.2 Development of a Cargo Aircraft, an Overview of the Preliminary Aerodynamic Design Phase
LI L. 1.5.2 Research on the Synthesis of Aircraft Configuration Parameters and Combat Effectiveness
LIMBERG W. 3.1.3 Transonic Flow Experiments with a 2-D Rectangular Wing Section Oscillating in Pitch
LIMNIOS N. 6.2.1 Maintenance Optimisation of a Digital Engine Control System with Limit Failure Rate Constrain
LIN J. 6.3.4 LEQG/LTR Controller Design with Extended Kalman Filter for Sensorless Induction Motor Servo Drive System
LIN M. 6.3.4 LEQG/LTR Controller Design with Extended Kalman Filter for Sensorless Induction Motor Servo Drive System
LIN Y. 7.6.3 The Development of a Low Cost Navigation System Using GPS/RDS Technology
LINCOLN J. W. 4.4.2 Effect of Aircraft Failures on USAF Structural Requirements
LIU J.L. 4.5.3 Deformation Inhomogeneity in a Single Crystal Nickel Base Superalloy
LIVERANI I. 6.6.R1 A Semi-Immersive Synthetic Environment for Cooperative Air Traffic Control
LODGE M. 3.11.1 Stability and Control of STOVL Aircraft
LOMBARDI G. 3.7.1 Numerical Analysis of Blockage Effects in Slotted Wind Tunnel
LORKOWSKI T. 4.9.4 Actuator Technology Based on Smart Materials for Adaptive Systems in Aerospace
LOU H.Y. 2.2.1 Airload Predictions for Delta Wings at High Incidence
LOVE J. F. 3.2.2 Aerodynamic Design and Analysis of a Reusable Launch Vehicle
LOVE M. 4.8.1 Computational Aeroelasticity in High Performance Aircraft Flight Loads
LOYAU H. 2.6.2 Numerical Investigation of Three-Dimensional Transonic Flow with Large Separation
LU C. J. 6.7.4 On the Correlation between Cultural Background and the Commercial Aircraft Accidents
LU W. 7.6.3 The Development of a Low Cost Navigation System Using GPS/RDS Technology
LUDLOW D. 2.4.2 Towards an Efficient Robust and Accurate Numerical Solver for Supersonic Viscous Flows
LUDLOW D.K. 2.4.3 Phantom Vorticity in Euler Solutions on Highly Stretched Grids
LUO X. 1.8.1 Experimental Study of No Tail Rotor (NOTAR) Helicopter
LUTTON M. 5.6.1 A CFD Applications to Store Sparation - Status Report
LUTZ Th. 2.11.1 Numerical Optimization of Adaptative Transonic Airfoils with Variable Camber
MACDIARMID I. 6.4.4 Cosmic Radiation Effects Upon Avionics - An Increasing Hazard in the New Millennium ?
MADDAH S. R. 2.9.R2 Experimental Investigation of Flowfield over a Multi-element Aerofoil and Comparison with Computational Prediction
MAGGIORE P. 1.7.4 An Academic Experience on Aircraft Design : Affordable Advanced Jet Trainer
MAILLE N. 6.7.2 REX : a Human Factor Flight Safety Research Program
MAINA M. 2.8.2 Study of Methods and Philosophies for Designing Hybrid Laminar Flow Wings
MALHERBE B. 4.11.3 Improvement of Crash Models of Large Aeronautical Structures
MANTER J. M. 4.3.2 Airframe Structures Technology for Future Systems
MARCHETTI D. 3.3.1   360° Surface Pressure Survey of an Advanced Trainer Aircraft Model by PSP Technique in DNW High Speed Tunnel
MARCHETTI M. 4.3.4 Global Residual Damage Evaluation of Impacted Sandwich Panels at Low Energy
MARESCA Ch. 3.1.2 Flow Velocity Investigation by Embedded Laser Doppler Velocimetry on 3D Oscillating Wings
MARGARIS D. P. 3.9.4 Influence of Arbitrary Vortical Wake Evolution on Flowfield and Noise Generation of Helicopter Rotors
MARODON F. 6.9.2 An In-Flight Investigation of Handley Page Jetstream Handling during Landing - Non Linear Aspects
MARTIN W. 4.9.R1 Fiberoptic Smart Sensing of Component Deformations in Adaptive Wings
MARTINEZ-VAL R. 1.1.3 Flying Wing Versus Conventional Transport Airplane : the 300 Seat Case
MARTZAKLIS G. S. 6.5.1 (IL) Reducing Aviation Weather Related Accidents Through High Fidelity Weather Information Distribution and Presentation
MASEFIELD O 5.7.4 Optimisation of the Aircraft Development Process in Small Aircraft Companies
MASELAND J.E.J. 2.7.4   Short Turn Around Parallel CFD to Predict Three Dimensional High Lift Flows Around a Transport Aircraft Powered by Ultra High by Pass Ratio Turbofan Engines
MASSARO G.M. 7.4.4 Multi Disciplinary Design of a High Aspect Ratio Gravity Control Hang Glider with Aeroelastically Enhanced Maneuverability
MATHIOUDAKIS K. 5.1.2 Implementation of a 3D LDA System for the Measurement of Turbulent Quantities in Complex Turbomachinery Flows-Demonstration of Performance in an Axisymmetric Free Jet
MATSUMOTO A. 3.4.3 Downstream Evolution of a Laminar Spot
MATSUSHIMA K. 2.1.3 Supersonic Inverse Design of Wings for the Full Configuration of Japanese SST
MATSUSHITA H. 4.10.R2 Model Modification of Transonic Aerodynamic Force on a High-Aspect Ratio Aeroelastic Wing and its Active Flutter
MAVRIS D. 1.4.4 Methodology for Examining the Simultaneous Impact of Requirements, Vehicle Characteristics, and Technologies on Military Aircraft Design
MAZAHERI K. 2.3.4 Three Dimensional Unstructured Grid Generation for Finite Volume Solution of Euler Equations
MCCLEERY S. 5.7.5 Product Maturity Through Partnership
MCGUIRK J. J. 6.8.1 The Numerical Simulation and Experimental Validation of Ventilation Flow and Fire Events in a Trent Nacelle Fire Zone
MCLEAN D. 4.10.R1 The Design of an Automatic Flight Control System for a Hypersonic Transport Aircraft
MEBARKI Y. 3.3.4 Pressure Sensitive Paints: from Laboratory to Wind Tunnel
MEE R. 1.11.3 In-Air Route Planning for Military Aircraft
MEIJER J. J. 4.6.1 (IL)   Perspectives of NLR Aeroelastic Methods to Predict Wing/Store Flutter and Dynamic Loads of Fighter Type Aircraft
MEINKE M. 2.1.2 Numerical Simulation of he Interaction of Side Flap Vortices and Engines Jets
MENDENHALL M. R. 3.2.2 Aerodynamic Design and Analysis of a Reusable Launch Vehicle
MIKAMI F. 2.9.3 Experimental Investigation of Three Dimensional Separated Flow over a Body of Revolution at High Angles of Attack
MILLAR M. 1.3.3 Configuration of an Unmanned Ground Effect Vehicle
MILLER D.N. 6.11.2 Active Inlet Flow Control Technology Demonstration
MOHANDAS P. 1.3.2 Design of Optimum Payloads to Meet the Mission Requirements of UAV Systems
MOKRY M. 3.7.R2 The Art and Science of Wind Tunnel Wall Interference : New Challenges
MORA-CAMINO F. 1.9.3 Trajectory Generation and Display for Free Flight
MORAVSZKI Cs. 6.4.2 Electronic Flight Display Development Supported by Commercial of the Shelf Tools
MORELLI M. 3.7.1 Numerical Analysis of Blockage Effects in Slotted Wind Tunnel
MORRIS A. J. 5.7.3 A Distributed Design Scenario for Aerospace
MOSS J. B. 6.8.1 The Numerical Simulation and Experimental Validation of Ventilation Flow and Fire Events in a Trent Nacelle Fire Zone
MOUZUNOV V.A. 4.6.3 Static Aeroelasticity Analysis in Transonic Flow
MUELLER J. 2.5.2 Numerical Analysis of the Unsteady Flow Above a Slender Delta Wing at Large Angles of Attack
MUELLER J. 3.5.1 Shock Wave/Boundary Layer Interaction
MUEMMLER R. 3.5.1 Shock Wave/Boundary Layer Interaction
MUHAMMAD H. 5.3.3 In-Flight Thrust Determination by Load Measurement on the Engine Mounting System
MUHARDI M. 5.3.3 In-Flight Thrust Determination by Load Measurement on the Engine Mounting System
MULLEN G.J. 6.9.2 An In-Flight Investigation of Handley Page Jetstream Handling during Landing - Non Linear Aspects
MULLENDER A. 6.8.1 The Numerical Simulation and Experimental Validation of Ventilation Flow and Fire Events in a Trent Nacelle Fire Zone
MULLENDER A. J. 6.8.2 Validation of Novel Low Temperature Fire Event Modelling Technique
MUNIN A. G. 3.9.R1 Efficiency of Ejector Devices and of Sound Absorbing Structures for Jet Noise Reduction
MUNRO C. 1.7.2 Integration of Subscale Flight Testing Design Education
MUSSAD A. 5.7.5 Product Maturity Through Partnership
NAE C. 2.10.4 Active Flow Control over a Circular Cylinder
NAE C. 2.6.R1 Numerical Simulation of a Synthetic Jet Actuator
NAING S. 5.9.2 Error Budgeting and the Design of Large Aerostructures
NAKAHASHI K. 2.6.3 Overset Unstructured Grid Method for Flow Simulations of Complex and Multiple Body Problems
NANGIA R.K. 1.6.1 Wing Design of an Oblique Wing Combat Aircraft
NANGIA R.K. 5.2.1 Civil Aircraft Engine Intakes with Negative Scarf Inspired by Requirements for Acoustic Reductions - Preliminary, Aerodynamic Performance Assessment
NARKIEWICZ J. 4.9.2 Comprehensive Modelling of Smart Structures for Aeroelastic Applications
NEAMTU M. 1.6.4 Lift at High Angle of Attack of a Fuselage Delta Wing Configuration with Canard Lateral Jets
NEBIOLO S. 2.6.4 A Propeller Integration Study Comparing Experimental Data with Numerical Flow Solutions Based on the Navier-Stokes Equations
NEELY A. 6.8.2 Validation of Novel Low Temperature Fire Event Modelling Technique
NEKHAMKINA O. 3.4.R1 On the Characteristics of Incompressible Turbulent Boundary Layers
NESTERENKO G. 4.4.R1 Comparison of Damage Tolerance of Integrally and Riveted Stiffened Structures
NISHIKAWA N. 2.9.3 Experimental Investigation of Three Dimensional Separated Flow over a Body of Revolution at High Angles of Attack
NOGUCHI M. 2.9.R1 Adverse Reynolds Number Effect on Maximum Lift of Two Dimensional Airfoils
NORATO M.O. 2.10.2 Flow Control Downstream of a Backward Facing Step
NYMAN J. 6.1.3 Complete Aircraft System Simulation for Aircraft Design - Paradigms for Modelling of Complex System
ODI R. A. 5.9.2 Error Budgeting and the Design of Large Aerostructures
OELKER H. C. 6.6.R2 On-line Simulation as a Measure to Increase Safety in Flight-Testing of High Performance Aircraft
OESTERHELD C.M. 1.4.5 Influence of Aeroelastic Effects on Preliminary Aircraft Design
OGLE T. 5.9.1 (IL) Agile Manufacturing Processes
OKAMOTO K. 7.3.4 Wave Rotor Gasdynamics for an Aeropropulsion System
OLKIN S. 4.4.1 Problems of Ensuring Structural Life of the Second Generation Supersonic Transport
OTTAVIANO S. 4.4.3 Durability Damage Tolerance and Environmentally Assisted Crack Propagation Characteristics of a Tig Welded Titanium Alloy
OVARI G. 1.5.3 Some Thoughts about Change of Fighters at Air Force of the East European Countries
ÖZ H. 1.4.1 Flexible Composite Wing with Internal Actuation for Roll Maneuver
PAFNUTIEV V. 7.7.2 Transonic Unsteady Separated Flow over Profile
PAGWIWOKO C. P. 4.8.R1   Bond Graphs For Dynamic Modeling of Aeroelastic Simulations
PALMER M.E. 5.2.1 Civil Aircraft Engine Intakes with Negative Scarf Inspired by Requirements for Acoustic Reductions - Preliminary, Aerodynamic Performance Assessment
PALMQVIST J. 1.11.1   NINS/NILS - A New Navigation and Landing System for JAS39 Gripen
PALMQVIST J. 6.6.4 System Safety of the Ordinary and Emergency Flight Data Display on the Gripen Color Displays
PAPANIKAS D. G. 3.9.4 Influence of Arbitrary Vortical Wake Evolution on Flowfield and Noise Generation of Helicopter Rotors
PARIKH P. C. 2.4.1 (IL) The NASA Tetrahedral Unstructured Software System
PASQUINO M. 7.4.5 Digital Mock-up : A Useful Tool in Aircraft Design
PATEK Z. 3.1.1 Wind Tunnel Testing of Performance Degradation of Ice Contaminated Airfoils
PATRIANAKOS G. 7.3.1 Quasi-Simultaneous Viscous Inviscid Interaction for Three Dimensional Turbulent Wing Flow
PAUL D. B. 4.3.2 Airframe Structures Technology for Future Systems
PAYNE K.H. 5.7.3 A Distributed Design Scenario for Aerospace
PECHLOFF A. 7.7.3 Numerical Simulation of a Pitching NACA 0012 Airfoil
PENG S. 6.7.4 On the Correlation between Cultural Background and the Commercial Aircraft Accidents
PENN D. 1.2.2 Development of a Cargo Aircraft, an Overview of the Preliminary Aerodynamic Design Phase
PEQUENO A. A. 2.3.3 Flow Simulation over a Complete Satellite Launcher with a Cluster Configuration
PERKOWSKI W. 1.8.3 Nonlinear Dynamic Model for Flexural Vibrations Analysis of a Supercritical Helicopter's Tail Rotor Drive Shaft
PERRY M.L. 3.7.5 Wind Tunnel Wall Constraint: Extension to Three Dimensions
PERSIANI F. 6.6.R1 A Semi-Immersive Synthetic Environment for Cooperative Air Traffic Control
PERUGINI P. 4.1.R1 Influence of Contact Phenomena on Embedded Delaminations Growth in Composite
PETRE B. 5.5.1 Temperature and Convective Heat Transfer Coefficient Profiles Downstream a Multiperforated Plate - Application to Combustion Chamber Cooling
PETTERSON K. 2.9.4 Slender Forebody Aerodynamics at High Alpha
PFITZNER M. 5.1.1 Development of an Aeroengine Secondary Air System Employing Vortex Reducers
PHILPOT M. 6.11.1   Future Challenges for Powerplant Aerodynamic Integration in Combat Aircraft
PIRZADEH S. 2.4.4 A Solution Adaptive Technique Using Tetrahedral Unstructured Grids
PIRZADEH S. Z. 2.4.1 (IL) The NASA Tetrahedral Unstructured Software System
PISTEK A. 4.2.1 Optimum Design of A Stiffened Panel Using the Method of Mathematical Programming
PISTEK L. 3.3.2 New Generation Portable Data Acquisition System
POKORADI L. 5.9.4 Mathematical Model Based Methods to Investigate Manufacturing Anomalies
POLL D.I.A. 2.9.4 Slender Forebody Aerodynamics at High Alpha
POWELL C. A. 3.9.1 (IL) NASA Subsonic Jet Transport Noise Reduction Research
PREISS A. 5.1.4 Advances in Turboengine Real-Time Simulation for Modern Control System Development
PREISSER J. S. 3.9.1 (IL) NASA Subsonic Jet Transport Noise Reduction Research
PRICE I. A. 3.7.2 Overcoming the Challenges of Designing Manufacturing and Testing of Cryogenic Wind Tunnel Models
PRINCE S.A. 2.4.3 Phantom Vorticity in Euler Solutions on Highly Stretched Grids
PUCAR P. 1.11.1   NINS/NILS - A New Navigation and Landing System for JAS39 Gripen
PYRZ J. 5.11.2 Customer Driven Development of Aircraft Cabin and Subsystem Concept
QIN N 2.4.2 Towards an Efficient Robust and Accurate Numerical Solver for Supersonic Viscous Flows
QIN N. 2.4.3 Phantom Vorticity in Euler Solutions on Highly Stretched Grids
QUIN N. 2.10.5 CFD Study of Shock Control at Cranfield
QUINIOU H. 6.10.4 Turbomachinery Design Used Intensive CFD
RAGHUNATHAN R. 2.3.R1 Simulation of 3-Dimensional Incompressible Cavity Flows
RAHMAWATI D. 2.5.3 Prediction of Aerodynamic - Lift Redistribution on Flexible Wing Structure Using Transonic Unsteady Aerodynamic Code - Ntrans
RAJBHANDARI S. 4.1.3 Optimisation of Cut-Outs in Fibre Composite Components Using Finite Element Methods
RECKSIEK R. 6.4.3 The Development of a Civilian Fly by Wire Flight Control System
REICHEL R. 6.4.R1   Modular Computer System for ATD (VFW 614)
REIMERDES H.G. 4.6.2 Design and Qualification Concepts for Flexible Wind Tunnel Wing Models
REINERS D. 6.4.5 Model Based Software Development and Code Generation for Avionic Systems
RICCI F. 1.3.1 Design and Development of a Low Altitude Unmanned Aerial Vehicle
RICCIO A. 4.1.R1 Influence of Contact Phenomena on Embedded Delaminations Growth in Composite
RICHARDSON D. 6.1.4 OBOGS Integration into a Turbo-Prop Trainer Aircraft
RICK H. 5.1.4 Advances in Turboengine Real-Time Simulation for Modern Control System Development
RINOIE K. 3.10.4 Studies on the Optimum Performance of Tapered Vortex Flaps
RINOIE K. 6.7.3 Workload Measurements for Operations under Simulated Single Pilot Instrument Flight Rules
RISEBOROUGH P. 3.6.4 Dynamic Control Aspects of the Shipboard Launch of Unmanned Air Vehicles
RODCHENKO T. 4.4.1 Problems of Ensuring Structural Life of the Second Generation Supersonic Transport
RODENBERGER C. M. 5.10.1 Global Integration and Management of 21st Century Fighters
RODRIGUEZ L. M. 5.5.2 Computer Program for Simplified Evaluation of Gas Radiation in Turbine Engine Enclosures
RODRIGUEZ T. 5.5.2 Computer Program for Simplified Evaluation of Gas Radiation in Turbine Engine Enclosures
RODZEWICZ M. 4.4.R2   Experimental Investigation of the Load Spectrum and Fatigue Tests of the PW-5 World Class Glider
ROHACS J. 1.5.3 Some Thoughts about Change of Fighters at Air Force of the East European Countries
ROHÁCS J. 6.4.2 Electronic Flight Display Development Supported by Commercial of the Shelf Tools
ROPER J. 3.5.2 Computation of a Dynamically Deployed Flap Employing Adaptive Body Recovery
ROSEMBLUM J. P. 2.5.1 (IL)   Unsteady CFD for Aircraft Design
ROSTAND Ph. 2.5.1 (IL)   Unsteady CFD for Aircraft Design
RUBIN T. 1.2.2 Development of a Cargo Aircraft, an Overview of the Preliminary Aerodynamic Design Phase
RUBINI P. A. 6.8.1 The Numerical Simulation and Experimental Validation of Ventilation Flow and Fire Events in a Trent Nacelle Fire Zone
RUIZ C.G. 5.4.1   Multidisciplinary Design of Fire Control and Missile Systems using a Knowledge Based Engineering Architecture
RUSSO C. 3.8.1 (IL)   Propulsion Emissions Research at NASA
RYZHOVA T. B. 4.5.2 Non Destructive Assessment of the Radial Clearance of the Bolted Joints in Aircraft Structures
SACHS G. 6.4.2 Electronic Flight Display Development Supported by Commercial of the Shelf Tools
SACHS G. 4.10.4 Path-Attitude Inconsonance in High Speed Flight and Related Path Control Issues
SACHS G. 6.9.3 Predictive Flight Path Displays for Improved Manual Control Performance
SADDINGTON A.J. 2.9.1 Comparison of Jet Induced Lift Loss for Single and Coaxial Jets
SADRI A. M. 2.10.3 The Interaction of a Synthetic Jet with a Turbulent Boundary Layer
SAITOH K. 4.10.R2 Model Modification of Transonic Aerodynamic Force on a High-Aspect Ratio Aeroelastic Wing and its Active Flutter
SALE R. 3.7.2 Overcoming the Challenges of Designing Manufacturing and Testing of Cryogenic Wind Tunnel Models
SALVETTI M.V. 3.7.1 Numerical Analysis of Blockage Effects in Slotted Wind Tunnel
SANDERSON C. 6.4.4 Cosmic Radiation Effects Upon Avionics - An Increasing Hazard in the New Millennium ?
SANGKHOL R. 4.9.R1 Fiberoptic Smart Sensing of Component Deformations in Adaptive Wings
SANTA I. 5.2.R1 The Effect of Water Ingestion on the Operation of the Gas Turbine Engine
SANTESSON R. 6.6.4 System Safety of the Ordinary and Emergency Flight Data Display on the Gripen Color Displays
SARIC W. 3.4.1 (IL) Transition on Swept Wings
SASONGKO R. A. 4.8.R1   Bond Graphs For Dynamic Modeling of Aeroelastic Simulations
SATO K. 2.10.R1 Improvement of Aerodynamic Characteristics of Next Generation SST Wing by Lateral Blowing
SATO K. 3.5.3 Experimental Study on Self Induced Excitation Phenomena of Opposing Jet in Supersonic Flow
SAUVINET F. 4.10.1 (IL) Longitudinal Active Stability : Key Issues for Future Large Transport Aircraft
SCARAMUZZINO F. 4.1.R1 Influence of Contact Phenomena on Embedded Delaminations Growth in Composite
SCHAFFNER P. R. 6.5.1 (IL) Reducing Aviation Weather Related Accidents Through High Fidelity Weather Information Distribution and Presentation
SCHMITT D. 5.10.2 Scenario Based Aircraft Design Evaluation
SCHNEEGANS A. 5.10.3 Scenario Based Aircraft Design Using Knowledge Based Software Methods
SCHNEIDER M. 4.8.2 Coupled Steady and Unsteady Aeroelastic Simulations in the Transonic Flight Regime
SCHOEP E. 1.1.3 Flying Wing Versus Conventional Transport Airplane : the 300 Seat Case
SCHOLZ D. 1.7.3 Computer Based Training in Aircraft Design Education
SCHRODER F. 1.10.3 Airborne Observation of Ice Accretion and Aircraft Performance In Artificial and Natural Supercooled Ice Clouds on Dornier 228 and 328 Aircraft
SCHRÖDER W. 2.1.2 Numerical Simulation of he Interaction of Side Flap Vortices and Engines Jets
SCHRÖDER W. 3.1.3 Transonic Flow Experiments with a 2-D Rectangular Wing Section Oscillating in Pitch
SCHUMACHER G. 5.3.1   Fan Blade Off-Design, Analysis and Testing of a New Aeroengine
SCHWEIGER J. 1.4.2   Theoretical Methods for Design and Interaction of Active Elements in Aerospace Structures
SCHWEIGER J. 4.7.4 A Carbon Composite Diverging Vertical Tail for Commercial Airplanes
SCOTT M. L. 4.1.3 Optimisation of Cut-Outs in Fibre Composite Components Using Finite Element Methods
SCOTT M.L. 1.3.2 Design of Optimum Payloads to Meet the Mission Requirements of UAV Systems
SEDAGHAT A. 4.6.4 Prediction of Non-Linear Aeroelastic Instabilities
SENNES U. 6.9.3 Predictive Flight Path Displays for Improved Manual Control Performance
SENSBURG O. 4.7.4 A Carbon Composite Diverging Vertical Tail for Commercial Airplanes
SERAUDIE A. 3.4.2 Effect of Sound on Laminar Turbulent Transition on Swept Wings
SERGHIDES V.C. 1.5.R1   Preliminary Design of an Advance Tactical Fighter
SEVERONI R. 4.3.4 Global Residual Damage Evaluation of Impacted Sandwich Panels at Low Energy
SEVINC E. 7.7.4   On the Calibration of 30x60 mm Trisonic Wind Tunnel at the Istanbul Technical University
SHAFER D. B. 6.5.1 (IL) Reducing Aviation Weather Related Accidents Through High Fidelity Weather Information Distribution and Presentation
SHAHZAD M. 1.9.3 Trajectory Generation and Display for Free Flight
SHARMA S. 5.7.5 Product Maturity Through Partnership
SHARP K. 4.4.4 The Significance of Laminar Corrosion Defects in Aircraft
SHAW J. 6.10.2 NASA’S ULTRA-EFFICIENT ENGINE TECHNOLOGY (UEET) PROGRAM/AEROPROPULSION TECHNOLOGY LEADERSHIP FOR THE 21ST CENTURY
SHAW R. J. 1.1.2 (IL) An Overview of NASA's High Speed Research Program
SHCHERBAN K. 4.4.1 Problems of Ensuring Structural Life of the Second Generation Supersonic Transport
SHEU D. 1.10.5   Intensity and Time Considerations in Microburst Penetration
SHIMBO Y. 3.3.3 Pressure Sensitive Paint Application at Large Production Wind Tunnels
SHKADOV L.M. 1.1.R2 Investigations on Possible Characteristics of FW Superhigh Seating Capacity Airplane
SIBILSKI K. 3.11.2 An Agile Aircraft Non-Linear Dynamics by Continuation Methods and Bifurcation Theory
SIEGLING H.F. 4.9.R1 Fiberoptic Smart Sensing of Component Deformations in Adaptive Wings
SILANTIEV V. A. 2.1.R1 Optimization of a Given Planform Lifting System at Supersonic Speed
SIMMONS M. J. 3.7.2 Overcoming the Challenges of Designing Manufacturing and Testing of Cryogenic Wind Tunnel Models
SIMPSON J. 1.4.2   Theoretical Methods for Design and Interaction of Active Elements in Aerospace Structures
SINHA A. 1.3.2 Design of Optimum Payloads to Meet the Mission Requirements of UAV Systems
SLAVIK S. 1.7.R1   The Role of the Workshop and Manufacture of Airplane Parts in Teaching Design
SMITH H. 1.1.4 College of Aeronautics Blended Wing Body Airliner Development ¨Program
SMRCEK L. 1.3.3 Configuration of an Unmanned Ground Effect Vehicle
SMRCEK L. 3.1.1 Wind Tunnel Testing of Performance Degradation of Ice Contaminated Airfoils
SMRCEK L. 1.7.1 Changing Education Requirements for Design Engineers
SOBOLEV A. F. 3.9.R1 Efficiency of Ejector Devices and of Sound Absorbing Structures for Jet Noise Reduction
SOBRY J.F. 4.11.3 Improvement of Crash Models of Large Aeronautical Structures
SOMMERER A. 2.11.1 Numerical Optimization of Adaptive Transonic Airfoils with Variable Camber
SOULARD A.J. 2.8.1 AeroStation - A COBRA Components Approach to Aerodynamic Design Framework
SOUMILLON S. 2.6.1 Navier-Stokes Calculations at Aerospatiale-Airbus for Aircraft Design
SOUTIS C. 4.1.2 Modelling of Damage in Fibre Reinforced Composite Laminates under Multiaxial In-plane Loading
SOUTIS C. 4.1.R2 Failure Analysis of Composite Laminates with an Open Hole under Bi-Axial Compression Tension Loading
SPAZZINI P.G. 2.10.2 Flow Control Downstream of a Backward Facing Step
SPEIJKER L. J.P. 6.5.2 Assessment of Wake Vortex Safety to Determine Adequately Safe Separation Distances
SPYROPOULOS A. J. 3.9.4 Influence of Arbitrary Vortical Wake Evolution on Flowfield and Noise Generation of Helicopter Rotors
SREWART C. D. 6.8.1 The Numerical Simulation and Experimental Validation of Ventilation Flow and Fire Events in a Trent Nacelle Fire Zone
SRITJAHJONO B.E. 5.3.3 In-Flight Thrust Determination by Load Measurement on the Engine Mounting System
STALEWSKI W. 1.8.R1 Development of New Generation Main and Tail Rotors Blade Airfoils
STANCIU V. 5.1.R1   Contributions on Generalising the Air Breathing Propulsion Systems; the Multiple Jet Engine
STAUDACHER W. 3.5.1 Shock Wave/Boundary Layer Interaction
STAUDIGEL L. 4.9.R1 Fiberoptic Smart Sensing of Component Deformations in Adaptive Wings
STEIJL R. 6.5.3 Wake Vortex Simulations Using A Parallel High-Order Accurate Navier-Stokes Solver
STETTNER M. 4.8.2 Coupled Steady and Unsteady Aeroelastic Simulations in the Transonic Flight Regime
STICH R. 4.10.4 Path-Attitude Inconsonance in High Speed Flight and Related Path Control Issues
STOICESCU M. 4.11.R2 A Point of View Regarding to Dynamic Analysis of an Aircraft Structure
STORM S. 4.9.4 Actuator Technology Based on Smart Materials for Adaptive Systems in Aerospace
STOUGH H. P. 6.5.1 (IL) Reducing Aviation Weather Related Accidents Through High Fidelity Weather Information Distribution and Presentation
STOW P. 6.10.1   Multi-Disciplinary Optimization Approaches to Propulsion System Design and Integration
STREIT Th. 1.1.R1 Three-Surface Aircraft - A Concept for Future Large Aircraft
STROHMAYER A. 5.10.2 Scenario Based Aircraft Design Evaluation
STROHMEYER D. 1.1.R1 Three-Surface Aircraft - A Concept for Future Large Aircraft
STURLAND I.M. 5.4.3 Design, Fabrication and Mechanical Issues Relating to the Use of Microengineered Devices in Future Guided Weapons
SU J. 2.1.1 Numerical Analysis of the Aerodynamics of the Aurora Aircraft by an Inviscid / Viscous Interaction Method
SUN Q. 4.4.5 Calendar Fatigue Life of Airframe Materials
SYAMSUDIN H. 5.7.3 A Distributed Design Scenario for Aerospace
SYMEONIDES G. 5.1.2 Implementation of a 3D LDA System for the Measurement of Turbulent Quantities in Complex Turbomachinery Flows-Demonstration of Performance in an Axisymmetric Free Jet
SZABOLCSI R. 5.9.4 Mathematical Model Based Methods to Investigate Manufacturing Anomalies
SZMELTER J. 1.3.4 Aerodynamic Aspects of Flapping Wing Micro Air Vehicles
SZODRUCH J. 5.7.1 (IL)   Aircraft Design Optimizing Operators, Environmental System and Manufacturing Requirements
TAKAMI Gou 3.5.3 Experimental Study on Self Induced Excitation Phenomena of Opposing Jet in Supersonic Flow
TALIB A.R. A. 6.8.2 Validation of Novel Low Temperature Fire Event Modelling Technique
TAO B. 4.9.1 Theoretical and Experimental Study on Shape Memory Alloy Torsion Actuator
TAO B. 4.9.R2 Development and Testing of an Adaptive Rotor System Based on Solid Actuation and Non Contact Signal Transmission Technology
TAYLOR N. 3.7.R1 The Use of Adaptive Wall Technology to Expand the Subsonic Operating Envelope of the DERA 8ft High Speed Wind Tunnel
TEENGEN U. 1.9.4   The Cockpit View of Air Traffic Management
TENHAVE H.B.G. 3.9.3 The Influence of Modelling A-Symmetric Lateral Track Dispersion on Aircraft Noise Level Predictions
TEWS H.J. 6.1.1 Test Practices for Next Generation Aircraft Cabin Systems
THEINER R. 1.7.R1   The Role of the Workshop and Manufacture of Airplane Parts in Teaching Design
THEUNISSEN E. 6.9.3 Predictive Flight Path Displays for Improved Manual Control Performance
THOMASSON P.G. 3.6.1 (IL) Modelling Simulation and Flight Test Experience in the Development of Unstable Robotic Aircraft
THOMPSON R. 3.2.3 Prediction of X-33 Aerodynamic and Aerothermodynamic Development
THOMSON R. S. 4.1.3 Optimisation of Cut-Outs in Fibre Composite Components Using Finite Element Methods
THORBECK J. 1.7.3 Computer Based Training in Aircraft Design Education
THORNE J. 5.7.3 A Distributed Design Scenario for Aerospace
TIMMS S. 5.9.1 (IL) Agile Manufacturing Processes
TISCHLER V. 4.7.4 A Carbon Composite Diverging Vertical Tail for Commercial Airplanes
TITI I. 7.2.3 Target Tracking with the Use of Neural Networks
TJATRA I. W. 2.5.3 Prediction of Aerodynamic - Lift Redistribution on Flexible Wing Structure Using Transonic Unsteady Aerodynamic Code - Ntrans
TJATRA I. W. 4.7.2 Optimization of Tapered Wing Structures With Aeroelastic Constraints
TOGASHI F. 2.6.3 Overset Unstructured Grid Method for Flow Simulations of Complex and Multiple Body Problems
TORMALM M. 3.11.3 The Use of Desktop Simulations in the Carefree Maneuvering Flight Test Program of JAS39 Gripen
TOURRETTE L. 2.6.1 Navier-Stokes Calculations at Aerospatiale-Airbus for Aircraft Design
TRUAX P.P. 6.11.2  
TRUNIN Y. 4.4.1 Problems of Ensuring Structural Life of the Second Generation Supersonic Transport
TRUSCOTT P. 6.4.4 Cosmic Radiation Effects Upon Avionics - An Increasing Hazard in the New Millennium ?
TRUTZEL M. 4.9.R1 Fiberoptic Smart Sensing of Component Deformations in Adaptive Wings
TSACH S. 1.2.2 Development of a Cargo Aircraft, an Overview of the Preliminary Aerodynamic Design Phase
TSUCHIYA T. 7.4.1 An Integrated Optimization for Conceptual Designs of Spaceplane
TURCANU D. 2.1.4 The Aerodynamic and Dynamic Ventral Fins Effects on a Jet Trainer
TURCHAK L. 5.6.2 Mathematical Modeling for Studying the Conditions of Air Ammunition Warfare
TZONG T. 2.7.5 Prediction of Aeroelastic Effects of Aircraft Configurations Including High Lift Systems
UCHIDA T. 4.7.5 Shock Stall Flutter a Two-Dimensional Airfoil
UEDA T. 4.7.R1 Ultra Light Wing Structure for High Altitude Long Endurance UAV
UEDA T. 6.6.2 Scattering Analysis for Wreckage of In-Flight Breakup
URSU F. 6.3.2   An Artificial Intelligence Based Synthesis of Electrohydraulic Servo
URSU I. 6.3.2   An Artificial Intelligence Based Synthesis of Electrohydraulic Servo
USO G.I. 2.10.2 Flow Control Downstream of a Backward Facing Step
VANBAREN G.B. 6.5.2 Assessment of Wake Vortex Safety to Determine Adequately Safe Separation Distances
VELDHUIS L.L.M. 2.6.4 A Propeller Integration Study Comparing Experimental Data with Numerical Flow Solutions Based on the Navier-Stokes Equations
VELDMAN A.E.P. 7.3.1 Quasi-Simultaneous Viscous Inviscid Interaction for Three Dimensional Turbulent Wing Flow
VELEY D.E. 1.4.1 Flexible Composite Wing with Internal Actuation for Roll Maneuver
VENKAYYA V. 4.7.4 A Carbon Composite Diverging Vertical Tail for Commercial Airplanes
VERESS A. 7.7.5 Simplified Theory on Mathematical Model of Axial Compressor Characteristics Working over Sound Speed
VIALA S. 2.6.1 Navier-Stokes Calculations at Aerospatiale-Airbus for Aircraft Design
VINELLI G. 7.5.1 Modelling of the Control of a Thrust Vectored Aircraft
VLOT A 4.5.R2 Towards Technology Readiness of Fibre Metal Laminates
VOEVODENKO N.V. 2.3.1 Numerical Tool for Specific Flight Regimes
VOGELESANG L.B. 4.5.R2 Towards Technology Readiness of Fibre Metal Laminates
VOGELS M.E.S. 3.9.3 The Influence of Modelling A-Symmetric Lateral Track Dispersion on Aircraft Noise Level Predictions
VULLIERME J. J. 5.5.1 Temperature and Convective Heat Transfer Coefficient Profiles Downstream a Multiperforated Plate - Application to Combustion Chamber Cooling
VURAL S. 7.7.4   On the Calibration of 30x60 mm Trisonic Wind Tunnel at the Istanbul Technical University
WAGNER S. 2.11.1 Numerical Optimization of Adaptive Transonic Airfoils with Variable Camber
WAN T. 6.5.R1 Flying Quality Study under the Influence of Clear Air Turbulence
WANG B. 4.4.5 Calendar Fatigue Life of Airframe Materials
WANG H. 1.3.R1 The Development of a Jet-UAV Conceptual Design Code
WANG H. 1.5.2 Research on the Synthesis of Aircraft Configuration Parameters and Combat Effectiveness
WANG H. 1.8.1 Experimental Study of No Tail Rotor (NOTAR) Helicopter
WANG Hs. 6.3.4 LEQG/LTR Controller Design with Extended Kalman Filter for Sensorless Induction Motor Servo Drive System
WANG S. 6.2.3 Interrelation Reliability Analysis of Fault Tolerant Flight Control System
WANG X. 7.4.2 Aerodynamic Configuration Design of Aircraft Using Multi-objective Genetic Algorithm
WANG Z. 4.5.R1 Predicting Fatigue Life Improvement In Cold Expanded Fastener Joints
WASCHKA W. 5.1.1 Development of an Aeroengine Secondary Air System Employing Vortex Reducers
WATAKI A. 6.6.2 Scattering Analysis for Wreckage of In-Flight Breakup
WEERTS U. 4.5.1 Mixed Mode Fracture Characterization of Adhesive Joints
WEINERFELT P. 2.11.3 Prediction of Lift Losses due to Surface Roughness by Means of a 2D Navier-Stokes Solver
WELLER T. 4.9.3 Active Control of Flexible Structures Based on Fuzzy Logic
WELTE D. 1.10.3 Airborne Observation of Ice Accretion and Aircraft Performance In Artificial and Natural Supercooled Ice Clouds on Dornier 228 and 328 Aircraft
WENDT B.J. 6.11.2 Active Inlet Flow Control Technology Demonstration
WETTERMANN M. 4.9.4 Actuator Technology Based on Smart Materials for Adaptive Systems in Aerospace
WHITE E. B. 3.4.1 (IL) Transition on Swept Wings
WHITE P. J. 3.7.2 Overcoming the Challenges of Designing Manufacturing and Testing of Cryogenic Wind Tunnel Models
WICHMANN G. 1.1.R1 Three-Surface Aircraft - A Concept for Future Large Aircraft
WIDMAIER K. 7.4.3 Conceptual Design and Optimization of a High Aspect Ratio UAV Wing Made of Composite Material
WILHITE A. W. 1.1.2 (IL) An Overview of NASA's High Speed Research Program
WILKINSON P.R. 5.11.3 Shaping The Successful Implementation of Human Factors Integration
WILLIAMSON A. 5.9.2 Error Budgeting and the Design of Large Aerostructures
WISE C. K. 5.10.1 Global Integration and Management of 21st Century Fighters
WLEZIEN R. 2.10.1 (IL) Micro Adaptive Flow Control
WOLF K. 4.1.1 Optimization of Composite Aircraft Panels Using Evolutionary Computation Methods
WOLFSHTEIN M. 3.4.R1 On the Characteristics of Incompressible Turbulent Boundary Layers
WONG P.C.W. 2.8.2 Study of Methods and Philosophies for Designing Hybrid Laminar Flow Wings
WOOD N. J. 3.2.1 Prediction of Separation Induced Buffet over Novel Wing Configurations
WOOD N. J. 2.10.3 The Interaction of a Synthetic Jet with a Turbulent Boundary Layer
WOODS M. I. 3.2.1 Prediction of Separation Induced Buffet over Novel Wing Configurations
WOTTON M.B. 5.9.3   Information Systems in Civil Aircraft Industry AIDA - An Airbus On-line System
WRIGHT J.R. 4.6.4 Prediction of Non-Linear Aeroelastic Instabilities
WRIGHT M. C.N. 3.7.4 Development of a Half Model Testing Capability at ETW
WRZESIEN S. 2.7.R1 Numerical Structural Analysis of Viscous Compressible Flow Past an Airfoil and Body of Revolution
WUBBEN F.J.M. 3.9.3 The Influence of Modelling A-Symmetric Lateral Track Dispersion on Aircraft Noise Level Predictions
XIONG K. 4.9.1 Theoretical and Experimental Study on Shape Memory Alloy Torsion Actuator
XU Y.B. 4.5.3 Deformation Inhomogeneity in a Single Crystal Nickel Base Superalloy
YAGUA L. C.Q. 2.3.3 Flow Simulation over a Complete Satellite Launcher with a Cluster Configuration
YAKIMENKO Oleg 6.6.1 Rapid on Board Prototyping of Near Optimal Spatial Trajectories for Pilot's Associate
YAMASAKI M. 4.7.5 Shock Stall Flutter a Two-Dimensional Airfoil
YANG M. 7.6.3 The Development of a Low Cost Navigation System Using GPS/RDS Technology
YANG Q. 4.4.5 Calendar Fatigue Life of Airframe Materials
YAO H. 2.3.R1 Simulation of 3-Dimensional Incompressible Cavity Flows
YERMAK Y.N. 4.10.5 New Solutions of the Problem of Optimal Injection Trajectories Based on Complex Investigation of Dynamics and Aerodynamics
YORK C.B. 7.4.R1 Buckling of Skew Plates with Continuity or Rotational Edge Restraint
YOSHIDA K. 2.9.R1 Adverse Reynolds Number Effect on Maximum Lift of Two Dimensional Airfoils
YUKIMURA I. 4.7.5 Shock Stall Flutter a Two-Dimensional Airfoil
ZADONSKY S.M. 4.10.5 New Solutions of the Problem of Optimal Injection Trajectories Based on Complex Investigation of Dynamics and Aerodynamics
ZAIDIBIN Z. M. 1.4.3 The Design and Fabrication of Top Secret - La Mouette's Rigi Hang Glider
ZALUDIN Z. 4.10.R1 The Design of an Automatic Flight Control System for a Hypersonic Transport Aircraft
ZAMMIT-MANGION D. 1.10.4 Design and Validation Using Flight Data of a Method for Predicting the Ground Run Required for Take-off
ZAMULA G. N. 4.2.2 Stability of Built-up Cylindrical Structures with Consideration of Plastic and Postbuckling Behavior of Thin Walled Components
ZAPHIRAKIS V. 5.1.2 Implementation of a 3D LDA System for the Measurement of Turbulent Quantities in Complex Turbomachinery Flows-Demonstration of Performance in an Axisymmetric Free Jet
ZARDA P.R. 5.4.1   Multidisciplinary Design of Fire Control and Missile Systems using a Knowledge Engineering Architecture
ZBIKOWSKI R. 1.3.4 Aerodynamic Aspects of Flapping Wing Micro Air Vehicles
ZEGHAL K. 1.9.2 Delegation of Separation Assurance to Aircraft : Towards a Framework for Analysing the Different Concepts and Underlying Principles
ZHANG C. 1.8.1 Experimental Study of No Tail Rotor (NOTAR) Helicopter
ZHANG J. H. 4.5.3 Deformation Inhomogeneity in a Single Crystal Nickel Base Superalloy
ZHANG J.B. 7.3.2 Effects of Treatment of the Source Terms in Turbulent Models on the Convergence Rate
ZHANG M. 5.3.4 Experimental Investigation of Static Internal Performance for an Axisymmetric Vectoring Thrust Nozzle (AVEN)
ZHANG X. 4.5.R1 Predicting Fatigue Life Improvement In Cold Expanded Fastener Joints
ZHAO J. 5.3.4 Experimental Investigation of Static Internal Performance for an Axisymmetric Vectoring Thrust Nozzle (AVEN)
ZHU Y. 2.10.5 CFD Study of Shock Control at Cranfield
ZURLO N. 2.10.2 Flow Control Downstream of a Backward Facing Step
ZUSMAN R. 4.2.R1 An Adaptative Finite Element Framework for Fatigue Crack Propagation
ZWAAN R.J. 4.11.1 Experimental Study of Nonlinear Vibrations of Thin-Walled Cylindrical Shells
ZWEBER J.V. 1.4.1 Flexible Composite Wing with Internal Actuation for Roll Maneuver