Paper Number | Paper Title | Authors | Session |
Link to the abstract
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1.1.1 (IL) | 2020 Vision : Prospects for Large Civil Aircraft Propulsion | N. T. Birch | 1.1 Subsonic and Supersonic Transport 1 | |
1.1.2 (IL) | An Overview of NASA's High Speed Research Program | A. W. Wilhite, R. J. Shaw | 1.1 Subsonic and Supersonic Transport 1 | |
1.1.3 | Flying Wing Versus Conventional Transport Airplane : the 300 Seat Case | R. Martínez-Val and E. Schoep | 1.1 Subsonic and Supersonic Transport 1 | |
1.1.4 | College of Aeronautics Blended Wing Body Airliner Development ¨Program | H. Smith | 1.1 Subsonic and Supersonic Transport 1 | |
1.1.R1 | Three-Surface Aircraft - A Concept for Future Large Aircraft | G. Wichmann, D. Strohmeyer, Th. Streit | 1.1 Subsonic and Supersonic Transport 1 | |
1.1.R2 | Investigations on Possible Characteristics of FW Superhigh Seating Capacity Airplane | V. E. Denisov, N. P. Buzoverya, B. I. Gurevich, A. L. Bolsunovsky, L. M. Shkadov | 1.1 Subsonic and Supersonic Transport 1 | |
1.2.1 (IL) | 728 : A New Family of Regional Transports Aircraft | R. Birrenbach | 1.2 Subsonic and Supersonic Transport 2 | |
1.2.2 | Development of a Cargo Aircraft, an Overview of the Preliminary Aerodynamic Design Phase | S. Tsach, S. Bauminger, M. Levin, D. Penn and T. Rubin | 1.2 Subsonic and Supersonic Transport 2 | |
1.2.R1 | Design Investigation of Variable Camber Flaps for High-Subsonic Airliners | J.P. Fielding | 1.2 Subsonic and Supersonic Transport 2 | |
1.3.1 | Design and Development of a Low Altitude Unmanned Aerial Vehicle | A. F. Accardo, F. Ricci, P. Basso | 1.3 Unmanned Vehicles 1 | |
1.3.2 | Design of Optimum Payloads to Meet the Mission Requirements of UAV Systems | A. K. Sinha, C. Bil, M. L. Scott and P. Mohandas | 1.3 Unmanned Vehicles 1 | |
1.3.3 | Configuration of an Unmanned Ground Effect Vehicle | M. Millar, L. Smrcek | 1.3 Unmanned Vehicles 1 | |
1.3.4 | Aerodynamic Aspects of Flapping Wing Micro Air Vehicles | J. Szmelter, R. Zbikowski | 1.3 Unmanned Vehicles 1 | |
1.3.R1 | The Development of a Jet-UAV Conceptual Design Code | H. Wang, H. Hung | 1.3 Unmanned Vehicles 1 | |
1.4.1 | Flexible Composite Wing with Internal Actuation for Roll Maneuver | N. S. Khot, J. V. Zweber and D. E. Veley, H. Öz, F. E. East ep | 1.4 Multidisciplinary Optimization | |
1.4.2 | Theoretical Methods for Design and Interaction of Active Elements in Aerospace Structures | J. SIMPSON, J. SCHWEIGER | 1.4 Multidisciplinary Optimization |
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1.4.3 | The Design and Fabrication of Top Secret - La Mouette's Rigi Hang Glider | Z. M. Zain | 1.4 Multidisciplinary Optimization | |
1.4.4 | Methodology for Examining the Simultaneous Impact of Requirements, Vehicle Characteristics, and Technologies on Military Aircraft Design | D. N. Mavris, D. DeLaurentis | 1.4 Multidisciplinary Optimization | |
1.4.5 | Influence of Aeroelastic Effects on Preliminary Aircraft Design | C. M. Oesterheld, W. Heinze, P. Horst | 1.4 Multidisciplinary Optimization | |
1.5.1 | High Altitude Long Endurance Aircraft | P. Kaempf | 1.5 Military Aircraft 1 |
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1.5.2 | Research on the Synthesis of Aircraft Configuration Parameters and Combat Effectiveness | Wang Heping, Li Leiji | 1.5 Military Aircraft 1 | |
1.5.3 | Some Thoughts about Change of Fighters at Air Force of the East European Countries | J. Rohacs, G. Óvari | 1.5 Military Aircraft 1 | |
1.5.R1 | Preliminary Design of an Advance Tactical Fighter | V.C. Serghides | 1.5 Military Aircraft 1 |
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1.6.1 | Wing Design of an Oblique Wing Combat Aircraft | R. K. Nangia, D. I. Greenwell | 1.6 Military Aircraft 2 | |
1.6.2 | Design Synthesis and Optimisation of an Advanced Short Take -off and Vertical Landing (ASTOVL) Combat Aircraft | J.P. Fielding, N. Kehayas | 1.6 Military Aircraft 2 | |
1.6.3 | Predicting the Effects of New Technologies on Aircraft Structural Mass : UCAV Case Study | P. A. Eustace, L.R. Jenkinson | 1.6 Military Aircraft 2 | |
1.6.4 | Lift at High Angle of Attack of a Fuselage Delta Wing Configuration with Canard Lateral Jets | M. Neamtu | 1.6 Military Aircraft 2 | |
1.7.1 | Changing Education Requirements for Design Engineers | D. P. Coldbeck, L. Smrcek | 1.7 Design Education | |
1.7.2 | Integration of Subscale Flight Testing Design Education | C. Munro, P. Berry, P. Krus | 1.7 Design Education | |
1.7.3 | Computer Based Training in Aircraft Design Education | D. Scholz, J. Thorbeck | 1.7 Design Education | |
1.7.4 | An Academic Experience on Aircraft Design : Affordable Advanced Jet Trainer | S. Chiesa, L. Borello, P. Maggiore | 1.7 Design Education | |
1.7.5 | University Development of A Derivative Aircraft Based on A Kit-Glider | G. E. Dorrington | 1.7 Design Education | |
1.7.R1 | The Role of the Workshop and Manufacture of Airplane Parts in Teaching Design | S. Slavik, R. Theiner | 1.7 Design Education |
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1.8.1 | Experimental Study of No Tail Rotor (NOTAR) Helicopter | Luo X., Zhang C., Wang H. | 1.8 Rotorcraft | |
1.8.2 | Aerodynamical and Dynamical Investigation of Helicopter Rotors | Tamás Gausz | 1.8 Rotorcraft | |
1.8.3 | Nonlinear Dynamic Model for Flexural Vibrations Analysis of a Supercritical Helicopter's Tail Rotor Drive Shaft | Z.Dzygadlo, W. Perkowski | 1.8 Rotorcraft | |
1.8.R1 | Development of New Generation Main and Tail Rotors Blade Airfoils | W. Kania, W. Stalewski | 1.8 Rotorcraft |
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1.2.3 | Propeller Airframe Aerodynamic Interference on Twin Engine Aircraft | S. G. Derishev | 1.2 Subsonic and Supersonic Transport 2 | |
2.1.1 | Numerical Analysis of the Aerodynamics of the Aurora Aircraft by an Inviscid / Viscous Interaction Method | J. Su, J.T. Conway | 2.1 3-D Complex Configurations - Lower Order Methods | |
2.1.2 | Numerical Simulation of he Interaction of Side Flap Vortices and Engines Jets | E. Fares, M. Meinke, W. Schröder | 2.1 3-D Complex Configurations - Lower Order Methods | |
2.1.3 | Supersonic Inverse Design of Wings for the Full Configuration of Japanese SST | K. Matsushima, T. Iwamiya, H. Ishikawa | 2.1 3-D Complex Configurations - Lower Order Methods | |
2.1.4 | The Aerodynamic and Dynamic Ventral Fins Effects on a Jet Trainer | S. Bogos, D. Turcanu | 2.1 3-D Complex Configurations - Lower Order Methods | |
2.1.R1 | Optimization of a Given Planform Lifting System at Supersonic Speed | V. A. Silantiev, A.V. Ignatieva | 2.1 3-D Complex Configurations - Lower Order Methods | |
2.10.1 (IL) | Micro Adaptive Flow Control | R. Wlezien | 2.10 Flow Control | |
2.10.2 | Flow Control Downstream of a Backward Facing Step | P. G. Spazzini, G. I. Uso, N. Zurlo, G. M. Di Cicca, M. O. Norato | 2.10 Flow Control | |
2.10.3 | The Interaction of a Synthetic Jet with a Turbulent Boundary Layer | A. Crook, W. J. Crowther and N. J. Wood | 2.10 Flow Control | |
2.10.4 | Active Flow Control over a Circular Cylinder | Catalin Nae | 2.10 Flow Control | |
2.10.5 | CFD Study of Shock Control at Cranfield | N Qin, Y Zhu and PR Ashill | 2.10 Flow Control | |
2.10.R1 | Improvement of Aerodynamic Characteristics of Next Generation SST Wing by Lateral Blowing | M. Kamishita, K. Karashima, S. Aso, K. Sato | 2.10 Flow Control | |
2.10.R2 | A New Concept for the Adaptive Shock and Boundary Layer Control on Transonic Flows about Airfoils | C. DIMA, P. de MATTEIS | 2.10 Flow Control |
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2.11.1 | Numerical Optimization of Adaptive Transonic Airfoils with Variable Camber | A. Sommerer, Th. Lutz, S. Wagner | 2.11 Wing Section Design | |
2.11.2 | Airfoil Design Optimisation using Navier-Stokes Equations and Simulated Annealing | S. L. Lee and M. Damodaran | 2.11 Wing Section Design | |
2.11.3 | Prediction of Lift Losses due to Surface Roughness by Means of a 2D Navier-Stokes Solver | Per Weinerfelt | 2.11 Wing Section Design | |
2.11.R1 | The Effect of Ice-Accretion on the Lateral Controlability | P. Fifka, Z. Ancik | 2.11 Wing Section Design | |
2.2.1 | Airload Predictions for Delta Wings at High Incidence | X. Z. Huang, H.Y. Lou and E.S. Hanff | 2.2 High Angle of Attack Solutions | |
2.2.2 | An Engineering Approach to the Calculation of Two and Three Dimensional Flows with Extensive Separation | T. Cebeci, F. Johnson, K. C. Chang and H. H. Chen | 2.2 High Angle of Attack Solutions | |
2.2.3 | The Characteristic Time Constant Approach for Mathematical Modelling of High Angle of Attack Aerodynamics | Goman M.G., Greenwell D.I., Khrabrov A.N. | 2.2 High Angle of Attack Solutions | |
2.3.1 | Numerical Tool for Specific Flight Regimes | N.V.Voevodenko | 2.3 Design Processes Using CFD 1 | |
2.3.2 | A Solution Adaptive Grid Method for Calculation of High Speed Flows around Blunt Body Configurations | A.R Jahangirian | 2.3 Design Processes Using CFD 1 | |
2.3.3 | Flow Simulation over a Complete Satellite Launcher with a Cluster Configuration | J. L.F. Azevedo , E. Basso , L. Camila Q. Yagua , A. P. Antunes | 2.3 Design Processes Using CFD 1 | |
2.3.4 | Three Dimensional Unstructured Grid Generation for Finite Volume Solution of Euler Equations | K. Mazaheri, S. Bodaghabadi | 2.3 Design Processes Using CFD 1 | |
2.3.R1 | Simulation of 3-Dimensional Incompressible Cavity Flows | H. Yao, R. Cooper, R. Raghunathan | 2.3 Design Processes Using CFD 1 | |
2.4.1 (IL) | The NASA Tetrahedral Unstructured Software System | N. T. Frink, S. Z. Pirzadeh, P. C. Parikh | 2.4 CFD Solvers | |
2.4.2 | Towards an Efficient Robust and Accurate Numerical Solver for Supersonic Viscous Flows | T J Birch, D K Ludlow, N Qin | 2.4 CFD Solvers | |
2.4.3 | Phantom Vorticity in Euler Solutions on Highly Stretched Grids | S. A. Prince, D. K. Ludlow, N. Qin | 2.4 CFD Solvers | |
2.4.4 | A Solution Adaptive Technique Using Tetrahedral Unstructured Grids | S. Z. Pirzadeh | 2.6 CFD for Complex Flows | |
2.4.5 | Accuracy of Gradient Computations for Aerodynamic Shape Optimisation Problems | M. Chevalier and M. Berggren | 2.4 CFD Solvers | |
2.6.1 | Navier-Stokes Calculations at Aerospatiale-Airbus for Aircraft Design | C. Gacherieu, R. Collercandy, P. Larrieu, S. Soumillon, L. Tourrette, S. Viala | 2.6 CFD for Complex Flows | |
2.6.2 | Numerical Investigation of Three-Dimensional Transonic Flow with Large Separation | M.A. Leschziner and H. Loyau | 2.4 CFD Solvers | |
2.6.3 | Overset Unstructured Grid Method for Flow Simulations of Complex and Multiple Body Problems | K. Nakahashi, F. Togashi | 2.6 CFD for Complex Flows | |
2.6.4 | A Propeller Integration Study Comparing Experimental Data with Numerical Flow Solutions Based on the Navier-Stokes Equations | L.L.M. Veldhuis , S. Nebiolo | 2.6 CFD for Complex Flows | |
2.6.R1 | Numerical Simulation of a Synthetic Jet Actuator | C. Nae | 2.6 CFD for Complex Flows | |
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 | S.A.Galpin | 2.7 3-D Configurations - High Order Methods | |
2.7.2 | Aerodynamic Design Using the Euler Adjoint Approach | M. R. Cross | 2.7 3-D Configurations - High Order Methods | |
2.7.3 | Nonlinear k-e Turbulence Modeling for Industrial Applications | M. Amato, P. Catalano | 2.7 3-D Configurations - High Order Methods | |
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 | J.E.J. Maselawd | 2.7 3-D Configurations - High Order Methods |
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2.7.5 | Prediction of Aeroelastic Effects of Aircraft Configurations Including High Lift Systems | K. C. Chang, H. H. Chen, T. Tzong and T. Cebeci | 2.7 3-D Configurations - High Order Methods | |
2.7.R1 | Numerical Structural Analysis of Viscous Compressible Flow Past an Airfoil and Body of Revolution | Z. Dzygadlo, S. Wrzesien | 2.7 3-D Configurations - High Order Methods | |
2.8.1 | AeroStation - A COBRA Components Approach to Aerodynamic Design Framework | C.Casties, A.Soulard, E.Chaput, L.Barrera, J.Huchard | 2.8 Design Processes using CFD 2 | |
2.8.2 | Study of Methods and Philosophies for Designing Hybrid Laminar Flow Wings | P. W. C. Wong, M. Maina | 2.8 Design Processes using CFD 2 | |
2.8.3 | Recent Progress on Powerplant / Airframe Integration at AEROSPATIALE-AIRBUS | A. Hurez | 2.8 Design Processes using CFD 2 | |
2.9.1 | Comparison of Jet Induced Lift Loss for Single and Coaxial Jets | A J Saddington & K Knowles | 2.9 Flow Separation & Entrainment | |
2.9.2 | Phenomena of Dynamic Stall on Swept Wings | J. Henkner | 2.9 Flow Separation & Entrainment | |
2.9.3 | Experimental Investigation of Three Dimensional Separated Flow over a Body of Revolution at High Angles of Attack | T. Ishide, N. Nishikawa and F. Mikami | 2.9 Flow Separation & Entrainment | |
2.9.4 | Slender Forebody Aerodynamics at High Alpha | K.Petterson & D.I.A.Poll | 2.9 Flow Separation & Entrainment | |
2.9.R1 | Adverse Reynolds Number Effect on Maximum Lift of Two Dimensional Airfoils | K. Yoshida, M. Noguchi | 2.9 Flow Separation & Entrainment | |
2.9.R2 | Experimental Investigation of Flowfield over a Multi-element Aerofoil and Comparison with Computational Prediction | H.H. BRUUN, S.R. MADDAH | 2.9 Flow Separation & Entrainment | |
3.1.1 | Wind Tunnel Testing of Performance Degradation of Ice Contaminated Airfoils | M.Holl, Z. Pátek, L. Smrcek | 3.1 Experimental Aerodynamics | |
3.1.2 | Flow Velocity Investigation by Embedded Laser Doppler Velocimetry on 3D Oscillating Wings | E. Berton, C. Allain, D. Favier, C. Maresca | 3.1 Experimental Aerodynamics | |
3.1.3 | Transonic Flow Experiments with a 2-D Rectangular Wing Section Oscillating in Pitch | C. Hillenherms, W. Limberg, W. Schröder | 3.1 Experimental Aerodynamics | |
3.1.4 | An Experimental Investigation of a Rectangular Jet Impinging on a Flat Surface Obliquely | H. Acar and V. Atli | 3.1 Experimental Aerodynamics | |
3.10.1 | Application of Dynamic Manipulation on the Forebody Vortices of a Schematic Aircraft Model | R. Lee, R. J. Kind, E. S. Hanff | 3.10 Vortex Aerodynamics | |
3.10.2 | Fin Buffet Load Alleviation Using an Actively Controlled Auxiliary Rudder at Sideslip | C. Breitsamter and B. Laschka | 3.10 Vortex Aerodynamics | |
3.10.3 | Requirements for Subscale Simulation of Delta-Wing Vortex Characteristics | L. E. Ericsson, M. E. Beyers | 3.10 Vortex Aerodynamics | |
3.10.4 | Studies on the Optimum Performance of Tapered Vortex Flaps | K. Rinoie | 3.10 Vortex Aerodynamics | |
3.10.5 | A Numerical Method to Simulate the Onset of Breakdown of an Unconfined Isolated Vortex Core | H. W. M. Hoeijmakers | 3.10 Vortex Aerodynamics |
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3.2.1 | Prediction of Separation Induced Buffet over Novel Wing Configurations | M. I. Woods, N. J. Wood | 3.2 Special Configurations | |
3.2.2 | Aerodynamic Design and Analysis of a Reusable Launch Vehicle | M. R. Mendenhall, H. S. Y. Chou, J. F. Love | 3.2 Special Configurations | |
3.2.3 | Prediction of X-33 Aerodynamic and Aerothermodynamic Development | R. A Thompson | 3.2 Special Configurations | |
3.3.1 | 360° Surface Pressure Survey of an Advanced Trainer Aircraft Model by PSP Technique in DNW High Speed Tunnel | D. Marchetti | 3.3 Data Acquisition |
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3.3.2 | New Generation Portable Data Acquisition System | I. Jebácek, L. Píštek, P. Hobza | 3.3 Data Acquisition | |
3.3.3 | Pressure Sensitive Paint Application at Large Production Wind Tunnels | Y. Shimbo, K. Asai, N. Komatsu | 3.3 Data Acquisition | |
3.3.4 | Pressure Sensitive Paints: from Laboratory to Wind Tunnel | Y. Mébarki | 3.3 Data Acquisition | |
3.4.1 (IL) | Transition on Swept Wings | E. B. White and W. S. Saric | 3.4 Transition & Turbulence | |
3.4.2 | Effect of Sound on Laminar Turbulent Transition on Swept Wings | S. Aubrun, A. Seraudie, D. Biron and D. Arnal | 3.4 Transition & Turbulence | |
3.4.3 | Downstream Evolution of a Laminar Spot | A. Matsumoto | 3.4 Transition & Turbulence | |
3.4.4 | On the Effects of a Installed Propeller Slipstream on a Wing Boundary Layer | F.M. Catalano | 3.4 Transition & Turbulence | |
3.4.5 | Transition Onset Predictions for High-Lift Configurations | R.M. Czerwiec, J.R. Edwards, and H.A.Hassan | 3.4 Transition & Turbulence | |
3.4.R1 | On the Characteristics of Incompressible Turbulent Boundary Layers | O. Nekhamkina, M. Wolfshtein, B. Aupoix | 3.4 Transition & Turbulence | |
3.5.1 | Shock Wave/Boundary Layer Interaction | J. Müller, R. Mümmler, W. Staudacher | 3.5 High Speed Separated Flow | |
3.5.2 | Computation of a Dynamically Deployed Flap Employing Adaptive Body Recovery | J. J. Roper, J. A. Edwards | 3.5 High Speed Separated Flow | |
3.5.3 | Experimental Study on Self Induced Excitation Phenomena of Opposing Jet in Supersonic Flow | K. Karashima, S.Aso, G. Takami and K.Sato | 3.5 High Speed Separated Flow | |
3.7.1 | Numerical Analysis of Blockage Effects in Slotted Wind Tunnel | G. Lombardi , M.V. Salvetti, M. Morelli | 3.7 Wind Tunnel Aerodynamics | |
3.7.2 | Overcoming the Challenges of Designing Manufacturing and Testing of Cryogenic Wind Tunnel Models | P.J. White, I.A. Price, M.J. Simmons, R.S. Sale | 3.7 Wind Tunnel Aerodynamics | |
3.7.3 | Ground Efect Testing Capabilities in the Filton 12' x 10' Low Speed Wind Tunnel | M.C.W. Evans | 3.7 Wind Tunnel Aerodynamics | |
3.7.4 | Development of a Half Model Testing Capability at ETW | M. C.N. Wright | 3.7 Wind Tunnel Aerodynamics | |
3.7.5 | Drag, Lift and Pitching Moment Increments due to the Wind Tunnel Wall Constraint : Extension to Three Dimensions | J. E. Hackett, K. R. Cooper, M. L. Perry | 3.7 Wind Tunnel Aerodynamics | |
3.7.5 | Wind Tunnel Wall Constraint: Extension to Three Dimensions | J. E. Hackett, K. R. Cooper, M. L. Perry | 3.7 Wind Tunnel Aerodynamics | |
3.7.R1 | The Use of Adaptive Wall Technology to Expand the Subsonic Operating Envelope of the DERA 8ft High Speed Wind Tunnel | N. Taylor, M. Mokry, M. Khalid | 3.7 Wind Tunnel Aerodynamics | |
3.7.R2 | The Art and Science of Wind Tunnel Wall Interference : New Challenges | N. Taylor, M. Mokry, M. Khalid | 3.7 Wind Tunnel Aerodynamics | |
5.6.1 | ACFD Applications to Store Sparation - Status Report | A. Cenko, M. Lutton | 5.6 Stores Separation Topics | |
5.6.2 | Mathematical Modeling for Studying the Conditions of Air Ammunition Warfare | L.Turchak, A. Belotserkovski, M. Kanevski, N. Baranov | 5.6 Stores Separation Topics | |
5.6.3 | New Methodologies in the Integrated Approach to External Store Separation Problem Optimisation of Camera Positioning for Flight Test | S. Barbero, R. Gemma, D. Girodo | 5.6 Stores Separation Topics |
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Paper Number | Paper Title | Authors | Session |
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2.5.1 (IL) | Unsteady CFD for Aircraft Design | J. Rosemblum, Ph. Rostand | 2.5 Unsteady CFD |
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2.5.2 | Numerical Analysis of the Unsteady Flow Above a Slender Delta Wing at Large Angles of Attack | J. Müller , D. Hummel | 2.5 Unsteady CFD | |
2.5.3 | Prediction of Aerodynamic - Lift Redistribution on Flexible Wing Structure Using Transonic Unsteady Aerodynamic Code - Ntrans | I W. Tjatra, M. Kadar, D. Rahmawati | 2.5 Unsteady CFD | |
4.1.1 | Optimization of Composite Aircraft Panels Using Evolutionary Computation Methods | P. Kaletta, K. Wolf | 4.1 Composite Materials; Design & Analysis | |
4.1.2 | Modelling of Damage in Fibre Reinforced Composite Laminates under Multiaxial In-plane Loading | C Soutis, M Kashtalyan, G.A.O. Davies | 4.1 Composite Materials; Design & Analysis | |
4.1.3 | Optimisation of Cut-Outs in Fibre Composite Components Using Finite Element Methods | R. S. Thomson , S. P. Rajbhandari and M. L. Scott | 4.1 Composite Materials; Design & Analysis | |
4.1.4 | Compression and Torsion Buckling Tests on Fiber Composite Cylinders | C. BisagniI | 4.1 Composite Materials; Design & Analysis |
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4.1.R1 | Influence of Contact Phenomena on Embedded Delaminations Growth in Composite | A. Riccio, F. Scaramuzzino, P. Perugini | 4.1 Composite Materials; Design & Analysis | |
4.1.R2 | Failure Analysis of Composite Laminates with an Open Hole under Bi-Axial Compression Tension Loading | C. Soutis | 4.1 Composite Materials; Design & Analysis | |
4.11.1 | Experimental Study of Nonlinear Vibrations of Thin-Walled Cylindrical Shells | L.Gunawan, R.J.Zwaan, A.W.H.Klompé | 4.11 Structural Dynamics | |
4.11.2 | A Parametric Study of Aircraft Landing-Impact with Emphasis on Nose-Gear Landing Design Conditions | D. H. Chester | 4.11 Structural Dynamics | |
4.11.3 | Improvement of Crash Models of Large Aeronautical Structures | B. Malherbe, B. Langrand, J.L. Charles, J.F. Sobry | 4.11 Structural Dynamics | |
4.11.R1 | Multiple Impact of a Single Bird Against the Intake of a Turbofan Experimental and Numerical Activity | M. Anghileri, L. Castelletti | 4.11 Structural Dynamics |
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4.11.R2 | A Point of View Regarding to Dynamic Analysis of an Aircraft Structure | I. Fuiorea, M. Stoicescu | 4.11 Structural Dynamics | |
4.2.1 | Optimum Design of A Stiffened Panel Using the Method of Mathematical Programming | Píštek A., Hobza P. | 4.2 Structural Analysis & Numerical Simulation | |
4.2.2 | Stability of Built-up Cylindrical Structures with Consideration of Plastic and Postbuckling Behavior of Thin Walled Components | G.N. Zamula, K.M. Ierusalimsky | 4.2 Structural Analysis & Numerical Simulation | |
4.2.3 | Local Postbuckling Analysis of Curved Aerospace Structures | M. Fischer, D. Kennedy | 4.2 Structural Analysis & Numerical Simulation | |
4.2.R1 | An Adaptative Finite Element Framework for Fatigue Crack Propagation | D. Givoli, R. Zusman | 4.2 Structural Analysis & Numerical Simulation | |
4.3.1 (IL) | Structural Optimization in Crashworthy Design | V. Giavotto | 4.3 Structural Design and Optimization |
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4.3.2 | Airframe Structures Technology for Future Systems | J. M. Manter and D. B. Paul | 4.3 Structural Design and Optimization | |
4.3.3 | The FFA Operational Loads Monitoring Program - Achievements and Problems | T. J. Barnes | 4.3 Structural Design and Optimization | |
4.3.4 | Global Residual Damage Evaluation of Impacted Sandwich Panels at Low Energy | L. Battilomo, M. Marchetti, R. Severoni | 4.3 Structural Design and Optimization | |
4.4.1 | Problems of Ensuring Structural Life of the Second Generation Supersonic Transport | Shcherban K.S, Dementyev A.D., Olkin S.I., Rodchenko T.S., Trunin Yu.P. | 4.4 Structural Integrity, Durability & Damage Tolerance | |
4.4.2 | Effect of Aircraft Failures on USAF Structural Requirements | J. W. Lincoln | 4.4 Structural Integrity, Durability & Damage Tolerance | |
4.4.3 | Durability Damage Tolerance and Environmentally Assisted Crack Propagation Characteristics of a Tig Welded Titanium Alloy | A. Lanciotti, L. Lazzeri, S. Ottaviano | 4.4 Structural Integrity, Durability & Damage Tolerance | |
4.4.4 | The Significance of Laminar Corrosion Defects in Aircraft | G. Clark, K. Sharp | 4.4 Structural Integrity, Durability & Damage Tolerance | |
4.4.5 | Calendar Fatigue Life of Airframe Materials | Wang B., Fan J., Sun Q. and Yang Q. | 4.4 Structural Integrity, Durability & Damage Tolerance | |
4.4.R1 | Comparison of Damage Tolerance of Integrally and Riveted Stiffened Structures | G. Nesterenko | 4.4 Structural Integrity, Durability & Damage Tolerance | |
4.4.R2 | Experimental Investigation of the Load Spectrum and Fatigue Tests of the PW-5 World Class Glider | M. Rodzewicz | 4.4 Structural Integrity, Durability & Damage Tolerance |
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4.5.1 | Mixed Mode Fracture Characterization of Adhesive Joints | U. Weerts, H. Kossira | 4.5 Materials & Joints | |
4.5.2 | Non Destructive Assessment of the Radial Clearance of the Bolted Joints in Aircraft Structures | T. B. Ryzhova | 4.5 Materials & Joints | |
4.5.3 | Deformation Inhomogeneity in a Single Crystal Nickel Base Superalloy | J.H. Zhang, J.L. Liu, T.J. Jin, Y.B. Xu, Z.Q. Hu | 4.5 Materials & Joints | |
4.5.R1 | Predicting Fatigue Life Improvement In Cold Expanded Fastener Joints | X. Zhang, Z. Wang, J. Gaerke | 4.5 Materials & Joints | |
4.5.R2 | Towards Technology Readiness of Fibre Metal Laminates | A. Vlot, L.B. Vogelesang, T.J. De Vries | 4.5 Materials & Joints | |
4.6.1 (IL) | Perspectives of NLR Aeroelastic Methods to Predict Wing/Store Flutter and Dynamic Loads of Fighter Type Aircraft | J. J. Meijer | 4.6 Aeroelasticity 1 |
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4.6.2 | Design and Qualification Concepts for Flexible Wind Tunnel Wing Models | M. Kämpchen , W. Jung , A. Dafnis , H.G. Reimerdes | 4.6 Aeroelasticity 1 | |
4.6.3 | Static Aeroelasticity Analysis in Transonic Flow | F.Z. Ishmuratov, S.I. Kuzmina, V.A. Mosunov | 4.6 Aeroelasticity 1 | |
4.6.4 | Prediction of Non-Linear Aeroelastic Instabilities | A. Sedaghat, J.E. Cooper, J. R. Wright and A.Y.T. Leung | 4.6 Aeroelasticity 1 | |
4.6.R1 | Nonlinear Elastic Constrained Multibody Systems - An Adaptive Time-Stepping Algorithm Based on the Time-Discontinuous Galerkin Scheme | J. G. Damilano | 4.6 Aeroelasticity 1 | |
4.7.1 (IL) | Progress in the Prediction and Analysis of Aeroservoelastic Instabilities on Large Civil Transport Aircraft | M.LACABANNE, A.LAPORTE | 4.7 Aeroelasticity 2 | |
4.7.2 | Optimization of Tapered Wing Structures With Aeroelastic Constraints | H. Djojodihardjo, I W. Tjatra, I. Harjanto | 4.7 Aeroelasticity 2 | |
4.7.3 | Flutter Analysis of Composite Wings Using Symbolic Computation | J.R. Banerjee, R. Butler | 4.7 Aeroelasticity 2 | |
4.7.4 | A Carbon Composite Diverging Vertical Tail for Commercial Airplanes | V. Venkayya, V. Tischler, O. Sensburg, and T. Schweiger | 4.7 Aeroelasticity 2 | |
4.7.5 | Shock Stall Flutter a Two-Dimensional Airfoil | M. Yamasaki, T. Uchida, I. Yukimura And K. Isogai | 4.7 Aeroelasticity 2 | |
4.7.R1 | Ultra Light Wing Structure for High Altitude Long Endurance UAV | Z. Goraj, T. Ueda | 4.7 Aeroelasticity 2 | |
4.8.1 | Computational Aeroelasticity in High Performance Aircraft Flight Loads | M. Love, T. De La Garza, E. Charlton, D. Egle | 4.8 Aeroelasticity 3 | |
4.8.2 | Coupled Steady and Unsteady Aeroelastic Simulations in the Transonic Flight Regime | M. Stettner, W. Haase, A. Eberle, J. Grashof, M. Schneider | 4.8 Aeroelasticity 3 | |
4.8.3 | Navier-Stokes Based Direct Numerical Aeroelastic Simulation | G. Britten, J. Ballmann | 4.8 Aeroelasticity 3 | |
4.8.R1 | Bond Graphs For Dynamic Modeling of Aeroelastic Simulations | C. P. Pagwiwoko, R.A. Sasongko | 4.8 Aeroelasticity |
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4.9.1 | Theoretical and Experimental Study on Shape Memory Alloy Torsion Actuator | Xiong K., Tao B., Jin J. | 4.9 Smart Structures | |
4.9.2 | Comprehensive Modelling of Smart Structures for Aeroelastic Applications | Janusz P. Narkiewicz | 4.9 Smart Structures | |
4.9.3 | Active Control of Flexible Structures Based on Fuzzy Logic | K. Cohen, T. Weller and J. Z. Ben-Asher | 4.9 Smart Structures | |
4.9.4 | Actuator Technology Based on Smart Materials for Adaptive Systems in Aerospace | P. Jänker, F. Hermle, T. Lorkowski, S. Storm, M. Wettemann, M. Gerle | 4.9 Smart Structures | |
4.9.R1 | Fiberoptic Smart Sensing of Component Deformations in Adaptive Wings | M. Trutzel, H.F. Siegling, D. Betz, R. Sangkhol, L. Staudigel, W. Martin, O. Krumpholz | 4.9 Smart Structures | |
4.9.R2 | Development and Testing of an Adaptive Rotor System Based on Solid Actuation and Non Contact Signal Transmission Technology | Y. Chen, B. Tao, W. Gao, R. Chen, Z. Gu | 4.9 Smart Structures |
Paper Number | Paper Title | Authors | Session |
Link to the Paper
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5.1.1 | Development of an Aeroengine Secondary Air System Employing Vortex Reducers | M. Pfitzner and W. Waschka | 5.1 Gas Turbine Systems | |
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 | G. Simeonides, V. Zaphirakis, K. Mathioudakis | 5.1 Gas Turbine Systems | |
5.1.3 | Inverse Design of Turbomachinery Airfoils Using the Navier Stokes Equations | B. Kaplan and S. Eyi | 5.1 Gas Turbine Systems | |
5.1.4 | Advances in Turboengine Real-Time Simulation for Modern Control System Development | A. Kreiner, S. Kopp, A. Preiss, W. Erhard, H. Rick | 5.1 Gas Turbine Systems | |
5.1.R1 | Contributions on Generalising the Airbreathing Propulsion Systems; the Multiple Jet Engine | V. Stanciu, I. Andrei | 5.1 Gas Turbine Systems |
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5.2.1 | Civil Aircraft Engine Intakes with Negative Scarf Inspired by Requirements for Acoustic Reductions - Preliminary, Aerodynamic Performance Assessment | R. K. Nangia, M. E. Palmer | 5.2 Aeroengine Inlets & Ingestion | |
5.2.2 | Vortex System and the Interference Between an Air Intake and the Ground | A. Karlsson , L. Fuchs | 5.2 Aeroengine Inlets & Ingestion | |
5.2.3 | Particle Ingestion in Engines of Military Transport Aircraft | T. BARDAGI | 5.2 Aeroengine Inlets & Ingestion |
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5.2.R1 | The Effect of Water Ingestion on the Operation of the Gas Turbine Engine | I. SANTA | 5.2 Aeroengine Inlets & Ingestion | |
5.3.1 | Fan Blade Off-Design, Analysis and Testing of a New Aeroengine | G. Schumacher | 5.3 Fans & Powerplant Installations |
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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 | B. Bernay | 5.3 Fans & Powerplant Installations | |
5.3.3 | In-Flight Thrust Determination by Load Measurement on the Engine Mounting System | H. Muhammad, Muhardi, W. Kuntjoro and B.E. Sritjahjono | 5.3 Fans & Powerplant Installation | |
5.3.4 | Experimental Investigation of Static Internal Performance for an Axisymmetric Vectoring Thrust Nozzle (AVEN) | Jin J., Zhao J., Zhang M., Lai C. | 5.3 Fans & Powerplant Installations | |
5.3.R1 | Thrust Vectoring Nozzle for Military Aircraft Engines | D. Ikaza, P.R. Zarda, C.G. Ruiz | 5.3 Fans & Powerplant Installations | |
5.5.1 | Temperature and Convective Heat Transfer Coefficient Profiles Downstream a Multiperforated Plate - Application to Combustion Chamber Cooling | B. Petre, E. Dorignac,J. J. Vullierme | 5.5 Turbines, Combustion & Heat Transfer | |
5.5.2 | Computer Program for Simplified Evaluation of Gas Radiation in Turbine Engine Enclosures | T. Rodríguez, L.M. Rodríguez | 5.5 Turbines, Combustion & Heat Transfer | |
5.5.3 | Heat Transfer in a 180Deg Turn Ribbed Square Channel | G. Cardone , T. Astarita and G. M. Carlomagno | 5.5 Turbines, Combustion & Heat Transfer | |
5.5.R1 | Two Dimensional Simulation of Nozzleless Solid Rocket Motor Internal Ballistics | A. Amoli, S.M.H. Karimian | 5.5 Turbines, Combustion & Heat Transfer |
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6.10.1 | Multi-Disciplinary Optimization Approaches to Propulsion System Design and Integration | P. Stow | 6.10 ISOABE |
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6.10.2 | NASA’S ULTRA-EFFICIENT ENGINE TECHNOLOGY (UEET) PROGRAM/AEROPROPULSION TECHNOLOGY LEADERSHIP FOR THE 21ST CENTURY | Robert J. Shaw | 6.10 ISOABE | |
6.10.3 | Propulsion-Airframe Integration Design, Analysis and Challenges going into the 21st Century | Kevin Early | 6.10 ISOABE | |
6.10.4 | Turbomachinery Design Used Intensive CFD | H. Joubert, H. Quiniou | 6.10 ISOABE | |
6.11.1 | Future Challenges for Powerplant Aerodynamic Integration in Combat Aircraft | M. Philpot | 6.11 PowerPlant Integration |
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6.11.2 | Active Inlet Flow Control Technology Demonstration | J.W. Hamstra, D.N. Miller, P.P. Truax, B.A Anderson, B.J. Wendt | 6.11 PowerPlant Integration | |
6.11.3 | F/A - 18 E/F - F414-GE-400 Propulsion System Integration | C. Hall | 6.11 PowerPlant Integration |
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Paper Number | Paper Title | Authors | Session |
Link to the Paper
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3.11.1 | Stability and Control of STOVL Aircraft | C. Fielding, M. Lodge | 3.11 Flight Dynamics of Highly Maneuverable Combat Vehicles | |
3.11.2 | An Agile Aircraft Non-Linear Dynamics by Continuation Methods and Bifurcation Theory | K. Sibilski | 3.11 Flight Dynamics of Highly Maneuverable Combat Vehicles | |
3.11.3 | The Use of Desktop Simulations in the Carefree Maneuvring Flight Test Program of JAS39 Gripen | M. Tormalm, M. Bergström | 3.11 Flight Dynamics of Highly Maneuverable Combat Vehicles | |
3.6.1 (IL) | Modelling Simulation and Flight Test Experience in the Development of Unstable Robotic Aircraft | P.G.Thomasson | 3.6 Unmanned Vehicles 2 | |
3.6.2 | Dynamics of High Altitude Long Endurance UAV | Z. Goraj | 3.6 Unmanned Vehicles 2 | |
3.6.3 | Unmanned Air Vehicles | S. Anderson | 3.6 Unmanned Vehicles 2 |
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3.6.4 | Dynamic Control Aspects of the Shipboard Launch of Unmanned Air Vehicles | Crump, M.R. , Riseborough, P. , Bil, C. , Hill, R. | 3.6 Unmanned Vehicles 2 | |
4.10.1 (IL) | Longitudinal Active Stability : Key Issues for Future Large Transport Aircraft | F. Sauvinet | 4.10 Flight Dynamics of Transport & Aerospace Vehicles | |
4.10.2 | Identification of the Aeroelastic Model of a Large Transport Aircraft for Control Law Design and Validation | C. Le Garrec, M. Humbert, M. Lacabanne | 4.10 Flight Dynamics of Transport & Aerospace Vehicles | |
4.10.3 | Minimum Emission Ascent and Descent Trajectories | M. Human | 4.10 Flight Dynamics of Transport & Aerospace Vehicles | |
4.10.4 | Path-Attitude Inconsonance in High Speed Flight and Related Path Control Issues | R. Stich, G. Sachs, T.H. Cox | 4.10 Flight Dynamics of Transport & Aerospace Vehicles | |
4.10.5 | New Solutions of the Optimal Injection Problems Based on Complex Investigation of Dynamics and Aerodynamics | A.S. Filatyev, Yu.N. Yermak, A.A. Golikov, S.M. Zadonsky | 4.10 Flight Dynamics of Transport & Aerospace Vehicles | |
4.10.5 | New Solutions of the Problem of Optimal Injection Trajectories Based on Complex Investigation of Dynamics and Aerodynamics | A.S. Filatyev, Yu.N. Yermak, A.A. Golikov, S.M. Zadonsky | 4.10 Flight Dynamics of Transport & Aerospace Vehicles | |
4.10.R1 | The Design of an Automatic Flight Control System for a Hypersonic Transport Aircraft | D. McLean, Z. Zaludin | 4.10 Flight Dynamics of Transport & Aerospace Vehicles | |
4.10.R2 | Model Modification of Transonic Aerodynamic Force on a High-Aspect Ratio Aeroelastic Wing and its Active Flutter | A. Fujimori, H. Matsushita, K. Saitoh | 4.10 Flight Dynamics of Transport & Aerospace Vehicles | |
6.9.1 (IL) | Recent Experience in Flight Testing for Pilot Induced Oscillations (PIO) on Transport Aircraft | B. P. Lee | 6.9 Handling Qualities & Piloting | |
6.9.2 | An In-Flight Investigation of Handley Page Jetstream Handling during Landing - Non Linear Aspects | G. Mullen, F. Marodon | 6.9 Handling Qualities & Piloting | |
6.9.3 | Predictive Flightpath Displays for Improved Manual Control Performance | E. Theunissen, U.Sennes and G.Sachs | 6.9 Handling Qualities & Piloting | |
6.9.4 | Neal-Smith Criteria-Based Hoo Approach to Predicting Aircraft Handling Qualities | N. Goto, T. Hoshizaki | 6.9 Handling Qualities & Piloting | |
6.9.R1 | Flying Qualities Design for a Fly-by-Wire Transport Aircraft in the Landing Flight Phase | J. Gautrey | 6.9 Handling Qualities & Piloting |
Paper Number | Paper Title | Authors | Session |
Link to the Paper
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6.1.1 | Test Practices for Next Generation Aircraft Cabin Systems | H.J. Tews et al. | 6.1 Aircraft Systems | |
6.1.2 | Insulation Concept & Material Optimisation in Business Aircraft | C. Bourban, R. Arndt | 6.1 Aircraft Systems | |
6.1.3 | Complete Aircraft System Simulation for Aircraft Design - Paradigms for Modelling of Complex System | P. Krus, J. Nyman | 6.1 Aircraft Systems | |
6.1.4 | OBOGS Integration into a Turbo-Prop Trainer Aircraft | D. Richardson | 6.1 Aircraft Systems | |
6.3.1 | Model Based Fault Detection for an Aircraft Actuator | P.Y. Crepin , R. Kress | 6.3 Controls & Actuators | |
6.3.2 | An Artificial Intelligence Based Synthesis of Electrohydraulic Servo | I. Ursu, F. Ursu | 6.3 Controls & Actuators |
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6.3.3 | Flow Control Electro-Hydraulic Servo Valve Assembly with in-Built Automatic Failure Detection and Compensation | J. J. Álvarez García | 6.3 Controls & Actuators | |
6.3.4 | LEQG/LTR Controller Design with Extended Kalman Filter for Sensorless Induction Motor Servo Drive System | J. Lin, Hs. Wang and M. Lin | 6.3 Controls & Actuators | |
6.4.1 (IL) | Human Centered Design Flight Deck Design and Utility System Integration | F. Blobner | 6.4 Flight Deck & Avionics |
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6.4.2 | Electronic Flight Display Development Supported by Commercial of the Shelf Tools | Cs. Moravszki, J. Rohács, P. Hermle and G. Sachs | 6.4 Flight Deck & Avionics | |
6.4.3 | The Development of a Civilian Fly by Wire Flight Control System | E. Kleemann, D. Dey, R. Recksiek | 6.4 Flight Deck & Avionics | |
6.4.4 | Cosmic Radiation Effects Upon Avionics - An Increasing Hazard in the New millennium ? | C Dyer, P Truscott, C Sanderson, B Colwell, A Chugg, R Jones, I MacDiarmid, K Johansson | 6.4 Flight Deck & Avionics | |
6.4.5 | Model Based Software Development and Code Generation for Avionic Systems | I. Fey, M. Hoffmann, D. Reiners | 6.4 Flight Deck & Avionics | |
6.4.R1 | Modular Computer System for ATD (VFW 614) | R. Reichel | 6.4 Flight Deck & Avionics |
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Paper Number | Paper Title | Authors | Session |
Link to the Paper
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5.10.1 | Global Integration and Management of 21st Century Fighters | C. K. Wise , C. M. Rodenberger | 5.10 Advanced Design and Development | |
5.10.2 | Scenario Based Aircraft Design Evaluation | A. Strohmayer, D. Schmitt | 5.10 Advanced Design and Development | |
5.10.3 | Scenario Based Aircraft Design Using Knowledge Based Software Methods | G. Dirks, A. Schneegans | 5.10 Advanced Design and Development | |
5.10.4 | The Latest Developments in Design Data Exchange : Towards Fully Integrated Aerospace Design Environments | J. Johnson | 5.10 Advanced Design and Development | |
5.10.5 | The Boeing Technical Research Center in Moscow - An Example of International Technology Development | S. Kravchenko | 5.10 Advanced Design and Development |
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5.11.1 | Systems Engineering in Marketing & Economics of Aero Engines | R. Dixon, L. Doukas | 5.11 Systems Engineering | |
5.11.2 | Customer Driven Development of Aircraft Cabin and Subsystem Concept | J. Pyrz | 5.11 Systems Engineering | |
5.11.3 | Shaping The Successful Implementation of Human Factors Integration | S.R. Harmer, J.L. Evans and P.R Wilkinson | 5.11 Systems Engineering | |
5.11.R1 | A Method for the Assessment of Technology Transparency | R. Edwards | 5.11 Systems Engineering |
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5.7.1 (IL) | Aircraft Design Optimizing Operators, Environmental System and Manufacturing Requirements | J. Szodruch | 5.7 Integrated Product Development |
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5.7.2 | Integrated Product Development - a Key to Affordability | G. Holmberg | 5.7 Integrated Product Development | |
5.7.3 | A Distributed Design Scenario for Aerospace | K. H. Payne, P. J. Deasley, H. Syamsudin, A. J. Morris, M. D. Guenov, J. P. Fielding, S. Evans & J. Thorne | 5.7 Integrated Product Development | |
5.7.4 | Optimisation of the Aircraft Development Process in Small Aircraft Companies | Oliver L.P. Masefield, A. Bruno Cervia | 5.7 Integrated Product Development | |
5.7.5 | Product Maturity Through Partnership | S. Sharma, A. Mussad, S. McCleery | 5.7 Integrated Product Development | |
5.9.1 (IL) | Agile Manufacturing Processes | S. Timms, T. Ogle, M. Jackson, C. Cooper | 5.9 Advanced Production Processes | |
5.9.2 | Error Budgeting and the Design of Large Aerostructures | R. Odi, G. Burley, S. Naing, A. Williamson, J. Corbett | 5.9 Advanced Production Processes | |
5.9.3 | Information Systems in Civil Aircraft Industry AIDA - An Airbus On-line System | M.B. Wotton | 5.9 Advanced Production Processes |
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5.9.4 | Mathematical Model Based Methods to Investigate Manufacturing Anomalies | L. PokorÁDi, R. Szabolcsi, J. Bera | 5.9 Advanced Production Processes |
Paper Number | Paper Title | Authors | Session |
Link to the Paper
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1.10.1 | An Information System for the Airport | M. Lemoine | 1.10 Airport/Weather | |
1.10.2 | On the Wake Vortex Hazard and Aircraft Safe Separation | L. M. B. C. Campos | 1.10 Airport/Weather |
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1.10.3 | Airborne Observation of Ice Accretion and Aircraft Performance In Artificial and Natural Supercooled Ice Clouds on Dornier 228 and 328 Aircraft | F. Scröder, D. Welte, T. Hauf | 1.10 Airport/Weather | |
1.10.4 | Design and Validation Using Flight Data of a Method for Predicting the Ground Run Required for Take-off | D. Zammit-Mangion, M. Eshelby | 1.10 Airport/Weather | |
1.10.5 | Intensity and Time Considerations in Microburst Penetration | J. Chern, D. Sheu | 1.10 Airport/Weather |
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1.11.1 | NINS/NILS - A New Navigation and Landing System for JAS39 Gripen | J. Palmqvist, P. Pucar, P. Bergljung | 1.11 Military Operations |
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1.11.2 | Training of Military Pilots | H. Eisenlohr | 1.11 Military Operations |
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1.11.3 | In-Air Route Planning for Military Aircraft | R. Mee | 1.11 Military Operations | |
1.9.1 | ASAS - Investigations Into Airborne Separation Assurance in a Distributed Simulation Environment | E. Brämer, O. Lehmann, H. Fricke, G. Hüttig | 1.9 Air Traffic Management | |
1.9.2 | Delegation of Separation Assurance to Aircraft : Towards a Framework for Analysing the Different Concepts and Underlying Principles | K. Zeghal, E. Hoffman | 1.9 Air Traffic Management | |
1.9.3 | Trajectory Generation and Display for Free Flight | M. Shahzad, F. Mora-Camino, J.. Slama and K. Achaibou | 1.9 Air Traffic Management | |
1.9.4 | The Cockpit View of Air Traffic Management | U. Teengen | 1.9 Air Traffic Management |
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Paper Number | Paper Title | Authors | Session |
Link to the Paper
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6.2.1 | Maintenance Optimisation of a Digital Engine Control System with Limit Failure Rate Constrain | M. Boussemart, T. Bickard, N. Limnios | 6.2 Safety of Fault Tolerant System | |
6.2.2 | Qualifications Chasing Avionics Technology? | I. Brodie | 6.2 Safety of Fault Tolerant System | |
6.2.3 | Interrelation Reliability Analysis of Fault Tolerant Flight Control System | S. Wang | 6.2 Safety of Fault Tolerant System | |
6.5.1 (IL) | Reducing Aviation Weather Related Accidents Through High Fidelity Weather Information Distribution and Presentation | H. P. Stough, D. B. Shafer, P.R. Schaffner, K. S. Martzaklis | 6.5 Safety in Adverse Atmospheric Conditions | |
6.5.2 | Assessment of Wake Vortex Safety to Determine Adequately Safe Separation Distances | L.J.P. Speijker, J. Kos, H.A.P. Blom, G.B. van Baren | 6.5 Safety in Adverse Atmospheric Conditions | |
6.5.3 | Wake Vortex Simulations Using A Parallel High-Order Accurate Navier-Stokes Solver | R. Steijl , H.W.M. Hoeijmakers | 6.5 Safety in Adverse Atmospheric Conditions | |
6.5.R1 | Flying Quality Study under the Influence of Clear Air Turbulence | T. Wan, C. Chen | 6.5 Safety in Adverse Atmospheric Conditions | |
6.6.1 | Rapid on Board Prototyping of Near Optimal Spatial Trajectories for Pilot's Associate | Oleg A. Yakimenko | 6.6 Safety Related Displays and Modelling | |
6.6.2 | Scattering Analysis for Wreckage of In-Flight Breakup | T. Ueda, A. Kanda and A. Wataki | 6.6 Safety Related Displays and Modelling | |
6.6.3 | Precipitation Drag of Snow and Standing Water | M. Giesberts, J. Gooden | 6.6 Safety Related Displays and Modelling | |
6.6.4 | System Safety of the Ordinary and Emergency Flight Data Display on the Gripen Color Displays | J. Palmqvist, R. Santesson | 6.6 Safety Related Displays and Modelling | |
6.6.R1 | A Semi-Immersive Synthetic Environment for Cooperative Air Traffic Control | F. Persiani, I. Liverani | 6.6 Safety Related Displays and Modelling | |
6.6.R2 | On-line Simulation as a Measure to Increase Safety in Flight-Testing of High Performance Aircraft | H. C. Oelker | 6.6 Safety Related Displays and Modelling | |
6.7.1 | Human Factors in Military Aircraft Accidents | J. Holroyo | 6.7 Human Factors Aspects of Aviation Safety |
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6.7.2 | REX : a Human Factor Flight Safety Research Program | N. Maille, L. Chaudron, P. Le Blaye, J.-Y. Grau | 6.7 Human Factors Aspects of Aviation Safety | |
6.7.3 | Workload Measurements for Operations under Simulated Single Pilot Instrument Flight Rules | K. Rinoie and K. Honda | 6.7 Human Factors Aspects of Aviation Safety | |
6.7.4 | On the Correlation between Cultural Background and the Commercial Aircraft Accidents | H. Jing, S. Peng, C. J. Lu | 6.7 Human Factors Aspects of Aviation Safety | |
6.8.1 | The Numerical Simulation and Experimental Validation of Ventilation Flow and Fire Events in a Trent Nacelle Fire Zone | A. J. Mullender, M. H. Coney, D. M. Horrocks, J. J. McGuirk, J. B. Moss, P. A. Rubini, C. D. Stewart and D. Binks | 6.8 Propulsion System Safety | |
6.8.2 | Validation of Novel Low Temperature Fire Event Modelling Technique | A.J. Neely, A.R.Abu Talib, P.T. Ireland, A.J. Mullender | 6.8 Propulsion System Safety | |
6.8.3 | A Stochastic Model of Friction Effected Degradation of Airborne Tribological Systems, as Used to Solve Diagnostic Problems | K. Bienczak | 6.8 Propulsion System Safety |
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Paper Number | Paper Title | Authors | Session |
Link to the Paper
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3.8.1 (IL) | Propulsion Emissions Research at NASA | C. Russo | 3.8 Aircraft Emissions |
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3.8.2 | Sustainable Aviation | J. J. Lee | 3.8 Aircraft Emissions | |
3.8.3 | The European Initiative Towards Ultra Low Emission Engines | K. Broichhausen | 3.8 Aircraft Emissions |
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3.9.1 (IL) | NASA Subsonic Jet Transport Noise Reduction Research | C. A. Powell, J. S. Preisser | 3.9 Aircraft Noise | |
3.9.2 | Airport Noise / Annoyance Analysis | M. Boyer , L. Chaudron | 3.9 Aircraft Noise | |
3.9.3 | The Influence of Modelling A-Symmetric Lateral Track Dispersion on Aircraft Noise Level Predictions | F.J.M. Wubben, M.E.S. Vogels, H.B.G. ten Have | 3.9 Aircraft Noise | |
3.9.4 | Influence of Arbitrary Vortical Wake Evolution on Flowfield and Noise Generation of Helicopter Rotors | A.J. Spyropoulos, A.P. Fragias, D.P. Margaris, D.G. Papanikas | 3.9 Aircraft Noise | |
3.9.R1 | Efficiency of Ejector Devices and of Soundabsorbing Structures for Jet Noise Reduction | V. M. Kouznetsov, A.G. Munin, A.F. Sobolev | 3.9 Aircraft Noise | |
3.9.R2 | Comparison of Prediction and Measurements on Propeller noise at an Angle of Attack | L.M.B.C. Campos, F.J.P. Lau | 3.9 Aircraft Noise |
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Paper Number | Paper Title | Authors | Session | Link to the Paper |
7.2.1 | Active Flutter Suppression for Nonlinear Aeroelastic System | T Degaki | 7.2 Flight Dynamics and Control 1 | |
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 | S. Kara, A. Guven | 7.2 Flight Dynamics and Control 1 | |
7.2.3 | Target Tracking with the Use of Neural Networks | I. Titi, A. Kaplan | 7.2 Flight Dynamics and Control 1 | |
7.3.1 | Quasi-Simultaneous Viscous Inviscid Interaction for Three Dimensional Turbulent Wing Flow | E.G.M. Coenen, A.E.P. Veldman and G. Patrianakos | 7.3 Aerodynamics 1 | |
7.3.2 | Effects of Treatment of the Source Terms in Turbulent Models on the Convergence Rate | J.B. Zhang | 7.3 Aerodynamics 1 | |
7.3.3 | PIV Study of Longitudinal Vortices in a Turbulent Boundary Layer Flow | G. M. Di Cicca | 7.3 Aerodynamics 1 | |
7.3.4 | Wave Rotor Gasdynamics for an Aeropropulsion System | K. Okamoto | 7.3 Aerodynamics 1 | |
7.4.1 | An Integrated Optimization for Conceptual Designs of Spaceplane | T. Tsuchiya | 7.4 Aerospace Design | |
7.4.2 | Aerodynamic Configuration Design of Aircraft Using Multi-objective Genetic Algorithm | Wang X., Gao Z. | 7.4 Aerospace Design | |
7.4.3 | Conceptual Design and Optimization of a High Aspect Ratio UAV Wing Made of Composite Material | K. Widmaier, F. M. Catalano | 7.4 Aerospace Design | |
7.4.4 | Multi Disciplinary Design of a High Aspect Ratio Gravity Control Hang Glider with Aeroelastically Enhanced maneuvarability | G. M. Massaro | 7.4 Aerospace Design | |
7.4.5 | Digital Mock-up : A Useful Tool in Aircraft Design | D. Camatti, S. Corpino, M. Pasquino | 7.4 Aerospace Design | |
7.4.R1 | Buckling of Skew Plates with Continuity or Rotational Edge Restraint | P. Huyton, C.B. York | 7.4 Aerospace Design | |
7.5.1 | Modelling of the Control of a Thrust Vectored Aircraft | G. Vinelli | 7.5 Flight Dynamics and Control 2 | |
7.5.2 | Mathematical Modelling of a Low Power Gas Turbine Engine and Its Control System | P. AilerI | 7.5 Flight Dynamics and Control 2 | |
7.5.3 | The Influence of Stealth Technology on Flight Performance and Maneuvering Characteristics of Fighter Aircraft | I. I. Ikryanov | 7.5 Flight Dynamics and Control 2 | |
7.6.1 | Use of Navigation Satellite Systems for Aircraft Operations : Sensitivity to Errors | JP Chauveau , B. Christophe, J. Lacroix | 7.6 Aircraft Operations and Safety | |
7.6.2 | Model of Degradation of Metal Polimeric Composite Joints in Aspect of Reliability and Safety | K. Kustron | 7.6 Aircraft Operations and Safety |
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7.6.3 | The Development of a Low Cost Navigation System Using GPS/RDS Technology | Y. Lin, W. Lu, M. Yang and F. Hsiao | 7.6 Aircraft Operations and Safety | |
7.7.1 | An Experimental Study on Wingtip Devices for Agricultural Aircraft | R. F. F. Coimbra and F. M. Catalano | 7.7 Aerodynamics 2 | |
7.7.2 | Transonic Unsteady Separated Flow over Profile | V. Pafnutiev | 7.7 Aerodynamics 2 | |
7.7.3 | Numerical Simulation of a Pitching NACA 0012 Airfoil | A. Pechloff | 7.7 Aerodynamics 2 | |
7.7.4 | On the Calibration of 30x60 mm Trisonic Wind Tunnel at the Istanbul Technical University | S. Vural, E. Sevinc, M.Z. Erim | 7.7 Aerodynamics 2 |
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7.7.5 | Simplified Theory on Mathematical Model of Axial Compressor Characteristics Working over Sound Speed | Á. Veress | 7.7 Aerodynamics 2 |