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This volume presents results of the interdisciplinary research work from the collaborative research center SFB 401: "Flow Modulation and Fluid-Structure Interaction at Airplane Wings" at RWTH Aachen, Germany The research reported here comprises work from the first five years of its funding by the Deutsche Forschungsgemeinschaft, DFG. The center is concerned with fundamental problems of very high capacity aircraft with large elastic wings capable of transonic transport. In all of the 14 projects to date, the following laboratories have cooperated: Aircraft Design and Aeronautics, Aerodynamics, Lightweight Structures, Flight Dynamics, Geometry and Practical Mathematics, Numerical Mathematics, Scientific Computing and Mechanics. The work is still in progress and presently approved to continue until the end of 2005.




This volume presents results of the interdisciplinary research work from the collaborative research center SFB 401: "Flow Modulation and Fluid-Structure Interaction at Airplane Wings" at RWTH Aachen, Germany The research reported here comprises work from the first five years of its funding by the Deutsche Forschungsgemeinschaft, DFG. The center is concerned with fundamental problems of very high capacity aircraft with large elastic wings capable of transonic transport. In all of the 14 projects to date, the following laboratories have cooperated: Aircraft Design and Aeronautics, Aerodynamics, Lightweight Structures, Flight Dynamics, Geometry and Practical Mathematics, Numerical Mathematics, Scientific Computing and Mechanics. The work is still in progress and presently approved to continue until the end of 2005.




This volume presents results of the interdisciplinary research work from the collaborative research center SFB 401: "Flow Modulation and Fluid-Structure Interaction at Airplane Wings" at RWTH Aachen, Germany The research reported here comprises work from the first five years of its funding by the Deutsche Forschungsgemeinschaft, DFG. The center is concerned with fundamental problems of very high capacity aircraft with large elastic wings capable of transonic transport. In all of the 14 projects to date, the following laboratories have cooperated: Aircraft Design and Aeronautics, Aerodynamics, Lightweight Structures, Flight Dynamics, Geometry and Practical Mathematics, Numerical Mathematics, Scientific Computing and Mechanics. The work is still in progress and presently approved to continue until the end of 2005.


Content:
Front Matter....Pages I-X
Introduction....Pages 1-3
Front Matter....Pages 5-5
Experimental Analysis and Modulation of Vortices....Pages 7-38
Simulation of Vortex Sheets at Take-Off and Landing....Pages 39-56
Analysis of Wakes and Wake-Jet Interaction....Pages 57-84
Aerodynamic Design of Transonic Adaptive Airfoils with Natural Transition....Pages 85-103
Experiments in a Transonic Shock Tube at Subsonic Mach and High Reynolds Numbers....Pages 105-122
Front Matter....Pages 123-123
H-Adaptive Multiscale Schemes for the Compressible Navier-Stokes Equations — Polyhedral Discretization, Data Compression and Mesh Generation....Pages 125-204
Automated Gradient Calculation....Pages 205-224
Front Matter....Pages 225-225
On Well-Posedness and Modelling for Nonlinear Aeroelasticity....Pages 227-247
Concepts for Reduced Structural Models of Airplane Wings in Aeroelasticity....Pages 249-273
Computational Aeroelasticity with Reduced Structural Models....Pages 275-299
Approximated Nonlinear Stability Analysis of the Dynamics of Flexible Aircraft....Pages 301-322
Analysis of Unsteady Airfoils at Low Speeds....Pages 323-350
Experiments on Transonic Aerodynamics about Elastically Suspended Airfoils....Pages 351-376
Design, Qualification and Experimental Investigation on Flexible Wind Tunnel Wing Models....Pages 377-396
Back Matter....Pages 397-398


This volume presents results of the interdisciplinary research work from the collaborative research center SFB 401: "Flow Modulation and Fluid-Structure Interaction at Airplane Wings" at RWTH Aachen, Germany The research reported here comprises work from the first five years of its funding by the Deutsche Forschungsgemeinschaft, DFG. The center is concerned with fundamental problems of very high capacity aircraft with large elastic wings capable of transonic transport. In all of the 14 projects to date, the following laboratories have cooperated: Aircraft Design and Aeronautics, Aerodynamics, Lightweight Structures, Flight Dynamics, Geometry and Practical Mathematics, Numerical Mathematics, Scientific Computing and Mechanics. The work is still in progress and presently approved to continue until the end of 2005.


Content:
Front Matter....Pages I-X
Introduction....Pages 1-3
Front Matter....Pages 5-5
Experimental Analysis and Modulation of Vortices....Pages 7-38
Simulation of Vortex Sheets at Take-Off and Landing....Pages 39-56
Analysis of Wakes and Wake-Jet Interaction....Pages 57-84
Aerodynamic Design of Transonic Adaptive Airfoils with Natural Transition....Pages 85-103
Experiments in a Transonic Shock Tube at Subsonic Mach and High Reynolds Numbers....Pages 105-122
Front Matter....Pages 123-123
H-Adaptive Multiscale Schemes for the Compressible Navier-Stokes Equations — Polyhedral Discretization, Data Compression and Mesh Generation....Pages 125-204
Automated Gradient Calculation....Pages 205-224
Front Matter....Pages 225-225
On Well-Posedness and Modelling for Nonlinear Aeroelasticity....Pages 227-247
Concepts for Reduced Structural Models of Airplane Wings in Aeroelasticity....Pages 249-273
Computational Aeroelasticity with Reduced Structural Models....Pages 275-299
Approximated Nonlinear Stability Analysis of the Dynamics of Flexible Aircraft....Pages 301-322
Analysis of Unsteady Airfoils at Low Speeds....Pages 323-350
Experiments on Transonic Aerodynamics about Elastically Suspended Airfoils....Pages 351-376
Design, Qualification and Experimental Investigation on Flexible Wind Tunnel Wing Models....Pages 377-396
Back Matter....Pages 397-398
....
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