《Advances in Simulation of Wing and Nacelle Stall》2014年

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《Advances in Simulation of Wing and Nacelle Stall: Results of the Closing Symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany》
在机翼和机舱失速模拟进展：结果DFG研究单位闭幕研讨会1066、十二月1-2，2014，不伦瑞克，德国
编者：
Rolf Radespiel
Reinhard Niehuis
Norbert Kroll
Kathrin Behrends
出版社：Springer
出版时间：2016年






目录
Part I: Modelling
The Delay of RANS-to-LES Transition in Hybrid RANS-LES
Approaches and Some Recently Proposed Remedies . . . . . . . . . . . . . . 3
Mikhail Strelets, Mikhail Shur, Andrey Travin, Philippe R. Spalart
Computations of Separated Flows with a Hybrid RANS/LES
Approach . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23
Daniela G. Francois, Rolf Radespiel, Silvia Reuß, Axel Probst
Hybrid RANS/LES Study of the Development
of an Airfoil-Generated Vortex. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41
Silvia Reuß, Axel Probst, Tobias Knopp, Katharina P. Wawrzinek
Interaction of Three-Dimensional Disturbances with the Flow
Around a Two-Element High-Lift Airfoil . . . . . . . . . . . . . . . . . . . . . . 55
Simon Klein, Peter Scholz, Rolf Radespiel
The Discontinuous Galerkin Method as an Enabling Technology
for DNS and LES of Industrial Aeronautical Applications. . . . . . . . . . 75
Koen Hillewaert, Corentin Carton de Wiart
Body Force Modelling of Internal Geometry for Jet Noise
Prediction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 97
James C. Tyacke, Iftekhar Z. Naqavi, Paul G. Tucker
Numerical Studies of Turbulent Flow Influence on a Two-Element
Airfoil. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 111
Katharina P. Wawrzinek, Thorsten Lutz, Ewald Krämer
CFD for Prediction of Flow Separation from Aircraft Tail Surfaces. . . 137
Andrea Masi, Jeremy Benton, Paul G. Tucker
Zonal RANS-LES Computation for Near-Stall-Airfoil Flow . . . . . . . . . 151
Benedikt Roidl, Koen J. Geurts, Wolfgang Schröder
Part II: Simulation of Atmospheric Disturbances
Criteria for Crosswind Variations during Approach and Touchdown
at Airports . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 167
Henk W. Krüs
Development and Improvement of Two Methods of Different
Complexity to Simulate Atmospheric Boundary Layer Turbulence
for Aircraft Design Studies. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 189
Christoph Knigge, Siegfried Raasch
Simulation of Interaction of Aircraft with Gust and Resolved
LES-Simulated Atmospheric Turbulence . . . . . . . . . . . . . . . . . . . . . . 203
Philip Kelleners, Ralf Heinrich
A New Method to Generate Anisotropic Synthetic Turbulence
for LES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 223
Torsten Auerswald, Jens Bange
Numerical Simulation of the Turbulent Flow Around a Wing . . . . . . . 235
Torsten Auerswald, Jens Bange
Part III: Inlet and Engine Flows
Integration- and Intake-Induced Flow Distortions and Their Impact
on Aerodynamic Fan Performance . . . . . . . . . . . . . . . . . . . . . . . . . . . 251
Rainer Schnell, Dirk Schönweitz, Marius Theune, Johakim Corroyer
Flow Investigations in a Stalling Nacelle Inlet under
Disturbed Inflow . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 271
Simon Übelacker, Rainer Hain, Christian J. Kähler
Realistic Inlet Distortion Patterns Interacting
with a Transonic Compressor Stage . . . . . . . . . . . . . . . . . . . . . . . . . . 285
Fabian Wartzek, Felix Holzinger, Christoph Brandstetter
, Heinz-Peter Schiffer
Unsteady CFD Simulation of Transonic Axial Compressor Stages
with Distorted Inflow. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 303
Sebastian Barthmes, Jakob P. Haug, Andreas Lesser, Reinhard Niehuis
VIII Contents
Transitional Shock-Wave/Boundary-Layer Interactions in Intakes
at Incidence. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 323
Tafara E. Makuni, Hardeep S. Kalsi, Paul G. Tucker, Holger Babinsky
Part IV: Applications in Complex Aircraft Flows
Advanced Design Approach for a High-Lift Wind Tunnel Model
Based on Flight Test Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 337
Niko Bier, Stefan Keye, David Rohlmann
Simulation of Longitudinal Vortices on a High-Lift Wing . . . . . . . . . . 351
Tim Landa, Jochen Wild, Rolf Radespiel
Impact of Different UHBR-Engine Positions on the Aerodynamics
of a High-Lift Wing. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 367
Sebastian Ritter
Numerical Investigation of the Influence of Pressure Belts
on the Stall of a Transport Aircraft in Landing Configuration . . . . . . 381
David Rohlmann
Numerical Studies of Active Flow Control Applied
at the Engine-Wing Junction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 397
Sebastian Fricke, Vlad Ciobaca, Jochen Wild, David Norman
Author Index . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 413

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