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《Flow Modulation and Fluid—Structure Interaction at Airplane Wings: Research Results of the Collaborative Research Center SFB 401 at RWTH Aachen, University of Technology, Aachen, Germany》
流调制和流体-结构相互作用在飞机的翅膀：对合作研究中心SFB 401在亚琛工业大学的研究成果，科技大学，亚琛，德国
编者：Josef Ballmann
出版社：Springer
出版时间：2003年
《Flow Modulation and Fluid—Structure Interaction at Airplane Wings: Research Results of the Collab ...
《Flow Modulation and Fluid—Structure Interaction at Airplane Wings: Research Results of the Collab ...
《Flow Modulation and Fluid—Structure Interaction at Airplane Wings: Research Results of the Collab ...
《Flow Modulation and Fluid—Structure Interaction at Airplane Wings: Research Results of the Collab ...
目录
Introduction
Model Flow, Wakes and Vortices in High Lift Configuration
2.1 Experimental Analysis and Modulation of Vortices
E. Özger, l. Schell, D. Jacob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
2.2 Simulation of Vortex Sheets at Take-Off and Landing
l. Schell, E. Özger, D. Jacob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 39
2.3 Analysis of Wakes and Wake-Jet Interaction
E. Fares, W. Schröder ..................................... 57
2.4 Aerodynamic Design of Transonic Adaptive Airfoils with Natural
Transition 85
A. Meijering, W. Limberg, W. Schröder ..................... .
2.5 Experiments in a Transonic Shock Tube at High Mach and
Reynolds Numbers
Th. ReicheI, M. Zechner, H. Olivier . . . . . . . . . . . . . . . . . . . . . . . . . 105
3 Numerical Tools and Approaches for Flow Simulation
4
with Local Adaptivity 123
3.1 H-Adaptive Multiscale Schemes for the Compressible NavierStokes
Equations - Polyhedral Discretization, Data Compression
and Mesh Generation
F. Bramkamp, B. Gottschlich-Müller, M. Hesse, Ph. Lamby,
S. Müller, J. Ballmann, K.H. Brakhage, W. Dahmen ........... 125
3.2 Automated Gradient Calculation
CH. Bischof, H.M. Bücker, B. Lang, A. Rasch. . . . . . . . . . . . . . . . 205
Computational and Experimental Aeroelasticity 225
4.1 On Well-Posedness and Modelling for Nonlinear Aeroelasticity
R. Massjung, J. Hurka, W. Dahmen, J. Ballmann ............. 227
4.2 Concepts for Reduced Structural Models of Airplane Wings in
Aeroelasticity
W. Jung, H.-G. Reimerdes .................................. 249
4.3 Computational Aeroelasticity with Reduced Structural Models
G. Britten, C Braun, M. Hesse, J. Ballmann ... . . . . . . . . . . . . . . 275
4.4 Approximated Nonlinear Stability Analysis of the Dynamics of
Flexible Aircraft
N. Siepenkötter, W. Kasberg, W. Alles. . . . . .. . . . . . . . . . . . . . . . . 301
IX
4.5 Analysis of Unsteady Airfoils at Low Speeds
x. Bertrdn, H. Olivier, S. Turek . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 323
4.6 Experiments on Transonic Aerodynamics about Elastically Suspended
Airfoils
C. Hillenherms, W. Schröder, W. Limberg . . . . . . . . . . . . . . . . . . . . 351
4.7 Design, Qualification and Experimental Investigation on Flexible
Wind-Tunnel Wing Models
M. Kämpchen, H. Korsch, A. Dafnis, H.-G. Reimerdes ........ 377
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