《MEGAFLOW - Numerical Flow Simulation for Aircraft Design》
《MEGAFLOW - Numerical Flow Simulation for Aircraft Design: Results of the second phase of the German CFD initiative MEGAFLOW, presented during its closing symposium at DLR, Braunschweig, Germany, December 10 and 11, 2002》MEGAFLOW-飞机设计的数值流模拟
编者:
Norbert Kroll
Jens K. Fassbender
出版社:Springer
出版时间:2005年
目录
Part I Grid Generation
1 Hybrid unstructured Grid Generation in MEGAFLOW
S. Melber-Wilkending, O. Brodersen, Y. Kallinderis, R. Wilhelm,
M. Sutcliffe, J. Wild, A. Ronzheimer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
Part II Structured Solver FLOWer
2 Block Structured Navier-Stokes Solver FLOWer
Jochen Raddatz, Jens K. Fassbender . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27
3 Transition Modeling in FLOWer — Transition Prescription
and Prediction
A. Krumbein . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 45
4 Turbulence Models in FLOWer
B. Eisfeld . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 63
Part III Hybrid Solver TAU
5 Overview of the Hybrid RANS Code TAU
Thomas Gerhold . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 81
6 Algorithmic Developments in TAU
Ralf Heinrich, Richard Dwight, Markus Widhalm, Axel Raichle . . . . . . . . 93
7 Hybrid Grid Adaptation in TAU
Thomas Alrutz . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 109
8 Turbulence Model Implementation in TAU
Keith Weinman . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 117
VIII Contents
9 G.I.G. — A Flexible User-Interface for CFD-Code
Configuration Data
Uwe Tapper . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 125
Part IV Validation
10 Computation of Aerodynamic Coefficients for Transport
Aircraft with MEGAFLOW
M. Rakowitz, S. Heinrich, A. Krumbein, B. Eisfeld, M. Sutcliffe . . . . . . . 135
11 Computation of Engine–Airframe Installation Drag
Olaf Brodersen . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 151
12 Verification of MEGAFLOW-Software for High Lift
Applications
S. Melber-Wilkending, R. Rudnik, A. Ronzheimer, T. Schwarz . . . . . . . . . 163
Part V Shape Optimization
13 The Continuous Adjoint Approach in Aerodynamic Shape
Optimization
N.R. Gauger, J. Brezillon . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 181
14 Application of the Adjoint Technique with the
Optimization Framework Synaps Pointer Pro
Jo¨el Brezillon. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 195
15 Shape Parametrization Using Freeform Deformation
Arno Ronzheimer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 211
Part VI Contributions of Universities
16 Advanced Turbulence Modelling in Aerodynamic Flow
Solvers
Martin Franke, Thomas Rung, Frank Thiele . . . . . . . . . . . . . . . . . . . . . . . . . 225
17 Large-Eddy Simulation of Attached Airfoil Flow
Qinyin Zhang, Matthias Meinke, Wolfgang Schr¨oder . . . . . . . . . . . . . . . . . . 241
18 Transition Prediction for 2D and 3D Flows using the
TAU-Code and N-Factor Methods
C. Nebel, R. Radespiel, R. Haas . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 251
Contents IX
Part VII Exploitation of MEGAFLOW Software
19 Application of the MEGAFLOW Software at DLR
R. Rudnik . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 269
20 MEGAFLOW for AIRBUS-D — Applications and
Requirements
Petra Aumann, Klaus Becker . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 283
21 Aerodynamic Analysis of Flapping Airfoil Propulsion at
Low Reynolds Numbers
Jan Windte, Rolf Radespiel, Matthias Neef, . . . . . . . . . . . . . . . . . . . . . . . . . 299
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