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《Computational Flight Testing：Results of the Closing Symposium of the German Research Initiative ComFliTe,Braunschweig, Germany, June 11th–12th,2012》
计算飞行测试：德国的研究comflite闭幕研讨会结果
作者：
Norbert Kroll
Rolf Radespiel
Jan Willem van der Burg
Kaare Sørensen (Eds.)
出版社：Springer
出版时间：2013年
《Computational Flight Testing：Results of the Closing Symposium of the German Research Initiative C ...
《Computational Flight Testing：Results of the Closing Symposium of the German Research Initiative C ...
《Computational Flight Testing：Results of the Closing Symposium of the German Research Initiative C ...
《Computational Flight Testing：Results of the Closing Symposium of the German Research Initiative C ...
目录
Innovative Algorithms
AMG in TAU: Adjoint Equations and Mesh Deformation . . . . . . . . . . . . . . 1
M. Förster, A. Pal
Accurate Simulation of Flows with Convected Vortices: Cartesian TAU . . 17
P. Kelleners
Turbulence and Transition Modeling
Hybrid RANS-LES Models . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27
K. Geurts, A. Probst
Investigation of the Resolution Requirements for a Hybrid RANS/LES
Simulation of a Multi-element Airfoil . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 43
S. Reuß, T. Knopp, D. Schwamborn
Improved Transition and Reynolds Stress Modeling in RANS Simulations 59
R.-D. Cécora, R. Radespiel, A. Probst
Simulation of Maximum Lift Using URANS for a High-Lift Transport
Configuration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75
J.W. van der Burg, M. Luehmann
Industrialization of the Automatic Transition Prediction in the DLR
TAU Code . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 89
N. Krimmelbein
Surrogate Modeling
Variable-Fidelity and Reduced-Order Models for Aero Data for Loads
Predictions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 99
S. Görtz, R. Zimmermann, Z.-H. Han
Response Surface Methods for Efficient Aerodynamic Surrogate Models . . 113
B. Rosenbaum, V. Schulz
Nonlinear Reduced Order Modeling for Aeroelastic Simulation with
Neural Networks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 131
K. Lindhorst, M.C. Haupt, P. Horst
Projection-Based Model Order Reduction for Steady Aerodynamics . . . . . 151
A. Vendl, H. Faßbender
VIII Table of Contents
Implementation of an Automatic Multi-fidelity Scheme for Industrial
Applications in the Cassidian SimServer Environment . . . . . . . . . . . . . . . . . 167
K. Sermeus, L. Nardin, K.A. Sørensen
Multidisciplinary Analysis
Modeling of Movable Control Surfaces and Atmospheric Effects . . . . . . . . . 183
L. Reimer, R. Heinrich
Coupling Strategies for Large Industrial Models . . . . . . . . . . . . . . . . . . . . . . . 207
J. Neumann, W. Krüger
NASTRAN Based Static CFD-CSM Coupling in FlowSimulator . . . . . . . . . 223
B. Stickan, H. Bleecke, S. Schulze
Industrial Applications
DLR Pilot Applications in ComFliTe . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 235
R. Heinrich, L. Reimer, A. Michler, B. Ernst, M. Ritter, J.
Neumann
Industrial ComFliTe Applications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 249
H. Bleecke, B. Stickan
Multi-component Modeling with the Dual Mesh Connect Approach. . . . . . 257
K.A. Sørensen
Transonic Tail Buffet Simulations on the ATRA Research Aircraft . . . . . . 273
S.A. Illi, T. Lutz, E. Krämer
Author Index . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 289
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