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 |