Initial
| 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 |
