RESERVE PAPERS
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1. INTEGRATION AND MULTIDISCIPLINARY MATTERS |
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1.1.R1 G. Wichmann, D. Strohmeyer, T. Streit, DLR, Braunschweig, Germany Three-Surface Aircraft - A Concept for Future Large Aircraft |
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1.1.R2 V. E. Denisov, N. P. Buzoverya, B. I. Gurevich, A. L. Bolsunovsky, L. M. Shkadov, Central Aerohydrodynamic Institute, Russia Investigations on Possible Characteristics of FW Superhigh Seating Capacity Airplane |
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1.2.R1 J. P. Fielding, College of Aeronautics, Cranfield University, UK Design Investigation of Variable Camber Flaps for High-Subsonic Airliners |
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1.3.R1 H. Wang, H. Hung, Northwestern Polytechnical University, Xi'an, PRC |
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1.5.R1 V. C. Serghides, Preliminary Design of an Advance Tactical Fighter |
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1.7.R1 S. Slavik, R. Theiner, The Role of the Workshop and Manufacture of Airplane Parts in Teaching Design |
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1.8.R1 W. Kania, W. Stalewski, Institute of Aviation, Poland Development of New Generation Main and Tail Rotors Blade Airfoils |
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2. AERODYNAMICS |
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2.1.R1 V. A. Silantiev, A.V. Ignatieva, SibNIA, Russia Optimization of a Given Planform Lifting System at Supersonic Speed |
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2.10.R1 M. Kamishita (1), K. Karashima (2), S. Aso (1), K. Sato (2), (1) Kyushu University; (2) Nishinippon Institute of Technology Improvement of Aerodynamic Characteristics of Next Generation SST Wing by Lateral Blowing |
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2.10.R2 C. DIMA, P. de MATTEIS, A New Concept for the Adaptive Shock and Boundary Layer Control on Transonic Flows about Airfoils |
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2.11.R1 P. Fifka, Z. Ancik, Brno University of Technology, Czech Republic |
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2.3.R1 H. Yao, R. Cooper, R. Raghunathan, The Queen’s University of Belfast, UK |
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2.6.R1 C. Nae, INCAS – National Institute for Aerospace Research, Romania |
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2.7.R1 Z. Dzygadlo, S. Wrzesien, Military University of Technology, Poland Numerical Structural Analysis of Viscous Compressible Flow Past an Airfoil and Body of Revolution |
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2.9.R1 K. Yoshida, M. Noguchi, NATIONAL AEROSPACE LABORATORY, Japan Adverse Reynolds Number Effect on Maximum Lift of Two Dimensional Airfoils |
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2.9.R2 H. H. BRUUN, S. R. MADDAH, University of Bradford, UK |
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3.4.R1 O. Nekhamkina, M. Wolfshtein, B. Aupoix, Technion – Israel Institute of Technology, Haifa, Israel On the Characteristics of Incompressible Turbulent Boundary Layers |
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3.7.R1 N. J. Taylor (1), P. R. Ashill, M. J. Simmons (3), (1) Matra BAe Dynamics Ltd., UK; (2) Cranfield University, UK; (3) DERA, UK |
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3.7.R2 M. Mokry, M. Khalid, Y. Mébarki, National Research Council Canada, Canada The Art and Science of Wind Tunnel Wall Interference : New Challenges |
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3. MATERIALS AND STRUCTURES |
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4.1.R1 A. Riccio (1), F. Scaramuzzino (2), P. Perugini (2), (1) Department of Aerospace Engineering, 2nd University of Naples, ITALY; (2) C.I.R.A. (Italian Aerospace Research Centre), ITALY Influence of Contact Phenomena on Embedded Delaminations Growth in Composite |
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4.1.R2 C. Soutis (1), P. T. Curtis (2), (1) Imperial College of Science, Technology and Medicine, London, UK; (2) DERA, UK Failure Analysis of Composite Laminates with an Open Hole under Bi-Axial Compression Tension Loading |
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4.11.R1 M. Anghileri, L. Castelletti, Multiple Impact of a Single Bird Against the Intake of a Turbofan Experimental and Numerical Activity |
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4.11.R2 I. Fuiorea, M. Stoicescu, Military Technical Academy, Bucharest, Romania A Point of View Regarding to Dynamic Analysis of an Aircraft Structure |
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4.2.R1 D. Givoli, R. Zusman, Technion — Israel Institute of Technology, ISRAEL An Adaptative Finite Element Framework for Fatigue Crack Propagation |
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4.4.R1 G. Nesterenko, TsAGI, Russia Comparison of Damage Tolerance of Integrally and Riveted Stiffened Structures |
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4.4.R2 M. Rodzewicz, Experimental Investigation of the Load Spectrum and Fatigue Tests of the PW-5 World Class Glider |
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4.5.R1 X. Zhang (1), Z. Wang (2), J. Gaerke (3), (1) College of Aeronautics, Cranfield University, UK; (2) Beijing Aeronautical Technology Research Centre, PRC; (3) Directorate of Technical Airworthiness, National Defence Headquarters, Canada Predicting Fatigue Life Improvement In Cold Expanded Fastener Joints |
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4.5.R2 J.W. Gunnink (1, 2), A. Vlot (2), R. C. Alderliesten (2), W. van der Hoeven (3), A. de Boer (3), W. ‘t Hart (3), C.G. van Hengel (1), P.L. Kuijpers (2), R.C. van Oost (1), G.H.J.J. Roebroeks (1), J. Sinke (2), M.S. Ypma (2), T.J. de Vries (2), Th. Wittenberg (2), (1) Structural Laminates Industries (an affiliate of Fokker Aerostructures), the Netherlands; (2) Delft University of Technology, 3 National Aerospace Laboratory (NLR), the Netherlands Towards Technology Readiness of Fibre Metal Laminates3. MATERIALS AND STRUCTURES |
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4.6.R1 J. G. Damilano, Instituto de Aeronáutica e Espaço, Centro Técnico Aeroespacial, CTA/IAE/ASE, BRAZIL |
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4.7.R1 Z. Goraj (1), T. Ueda (2), (1) Warsaw University of Technology, Warsaw, Poland; (2) Tetsuhiko Ueda, National Aeronautical Laboratory, Tokyo, Japan Ultra Light Wing Structure for High Altitude Long Endurance UAV |
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4.8.R1 C. P. Pagwiwoko, R.A. Sasongko, Bond Graphs For Dynamic Modeling of Aeroelastic Simulations |
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4.9.R1 M. Trutzel (1), H. F. Siegling (1), D. Betz (1), R. Sangkhol (1), L. Staudigel (1), W. Martin (2), O. Krumpholz (1), DaimlerChrysler AG, Research and Technology, Germany; (1) Optical Interconnects and Optical Sensors (FT2/HV), Ulm; (2) Structural Materials (FT4/W), Munich Fiberoptic Smart Sensing of Component Deformations in Adaptive Wings |
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4.9.R2 Y. Chen (1), B. Tao (1), W. Gao (2), R. Chen (2), Z. Gu (3), (1) National Engineering Research Center of Turbo-generator Vibration, Southeast University, Nanjing, PRC; (2) The Aeronautical Lab for Smart Materials & Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, PRC (3) National Lab of Rotor Aerodynamics, Nanjing University of Aeronautics and Astronautics, Nanjing, PRC |
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4. PROPULSION |
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5.1.R1 V. Stanciu, I. Andrei, Contributions on Generalising the Airbreathing Propulsion Systems; the Multiple Jet Engine |
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5.2.R1 I. SANTA, Technical University of Budapest, Hungary The Effect of Water Ingestion on the Operation of the Gas Turbine Engine |
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5.3.R1 D. Ikaza, P.R. Zarda, C. G. Ruiz, |
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5.5.R1 A. Amoli, S. M. H. Karimian, Two Dimensional Simulation of Nozzleless Solid Rocket Motor Internal Ballistics |
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5. FLIGHT DYNAMICS AND CONTROL |
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4.10.R1 D. McLean (1), Z. Zaludin (2), (1) University of Southampton, UK; (2) Universiti Putra, Malaysia The Design of an Automatic Flight Control System for a Hypersonic Transport Aircraft |
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5. FLIGHT DYNAMICS AND CONTROL |
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4.10.R2 A. Fujimori (1), H. Matsushita (2), K. Saitoh (2), (1) Department of Mechanical Engineering, Shizuoka University, Japan; (2) National Aerospace Laboratory, Japan |
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6.9.R1 J. Gautrey, College of Aeronautics, Cranfield University, UK Flying Qualities Design for a Fly-by-Wire Transport Aircraft in the Landing Flight Phase |
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6. SYSTEMS, SUBSYSTEMS AND EQUIPMENT |
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6.4.R1 R. Reichel, Modular Computer System for ATD (VFW 614) |
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7. DESIGN, DEVELOPMENT, MANUFACTURING AND MANAGEMENT |
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5.11.R1 R. Edwards, A Method for the Assessment of Technology Transparency |
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9. SAFETY |
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6.5.R1 T. Wan, C. Chen, Department of Aerospace Engineering, Tamkang University, Taipei, Taiwan, ROC. Flying Quality Study under the Influence of Clear Air Turbulence |
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6.6.R1 F. Persiani, I. Liverani, DIEM - Università di Bologna, v.le Risorgimento, 2, 40136 Bologna – Italy A Semi-Immersive Synthetic Environment for Cooperative Air Traffic Control |
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6.6.R2 H. C. Oelker (1), Thomas Meyer (2), (1) DaimlerChrysler Aerospace AG (2) Military Aircraft Division On-line Simulation as a Measure to Increase Safety in Flight-Testing of High Performance Aircraft |
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10. ENVIRONMENT |
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3.9.R1 V. M. Kouznetsov, A. G. Munin, A. F. Sobolev, Central Aerohydrodynamics Institute (TsAGI), Russia Efficiency of Ejector Devices and of Soundabsorbing Structures for Jet Noise Reduction |
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3.9.R2 L. M. B. C. Campos, F. J. P. Lau, Comparison of Prediction and Measurements on Propeller noise at an Angle of Attack |
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11. STUDENT SESSION |
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7.4.R1 P. Huyton, C. B. York, The University of Edinburgh, Edinburgh, UK Buckling of Skew Plates with Continuity or Rotational Edge Restraint |