Advances in simulation of wing and nacelle stall [electronic resource] : results of the closing symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany / edited by Rolf Radespiel, Reinhard Niehuis, Norbert Kroll, Kathrin Behrends.
Radespiel, Rolf, editor.; Niehuis, Reinhard, editor.; Kroll, Norbert, editor.; Behrends, Kathrin, editor.
2015
TL672
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Title Advances in simulation of wing and nacelle stall [electronic resource] : results of the closing symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany / edited by Rolf Radespiel, Reinhard Niehuis, Norbert Kroll, Kathrin Behrends.
ISBN 9783319211275 (electronic book)
3319211277 (electronic book)
9783319211268
Published [Cham] : Springer, [2015]
Copyright ©2016
Language English
Description 1 online resource (ix, 413 pages) : illustrations.
Call Number TL672
Dewey Decimal Classification 629.134/32
Summary The book reports on advanced solutions to the problem of simulating wing and nacelle stall, as presented and discussed by internationally recognized researchers at the Closing Symposium of the DFG Research Unit FOR 1066. Reliable simulations of flow separation on airfoils, wings and powered engine nacelles at high Reynolds numbers represent great challenges in defining suitable mathematical models, computing numerically accurate solutions and providing comprehensive experimental data for the validation of numerical simulations. Additional problems arise from the need to consider airframe-engine interactions and inhomogeneous onset flow conditions, as real aircraft operate in atmospheric environments with often-large distortions. The findings of fundamental and applied research into these and other related issues are reported in detail in this book, which targets all readers, academics and professionals alike, interested in the development of advanced computational fluid dynamics modeling for the simulation of complex aircraft flows with flow separation.
Bibliography, etc. Note Includes bibliographical references and author index.
Access Note Access limited to authorized users.
Source of Description Online resource; title from title details screen (SpringerLink, viewed July 17, 2015).
Added Author Radespiel, Rolf, editor.
Niehuis, Reinhard, editor.
Kroll, Norbert, editor.
Behrends, Kathrin, editor.
Series Notes on numerical fluid mechanics and multidisciplinary design ; volume 131.
Available in Other Form 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.
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The Delay of RANS-to-LES Transition in Hybrid RANS-LES Approaches and Some Recently Proposed Remedies
Computations of Separated Flows with a Hybrid RANS/LES Approach
Hybrid RANS/LES Study of the Development of an Airfoil-Generated Vortex
Interaction of Three-Dimensional Disturbances with the Flow around a Two-Element High-Lift Airfoil
The Discontinuous Galerkin Method as an Enabling Technology for DNS and LES of Industrial Aeronautical Applications
Body Force Modelling of Internal Geometry for Jet Noise Prediction
Numerical Studies of Turbulent Flow Influence on a Two-Element Airfoil
CFD for Prediction of Flow Separation from Aircraft Tail Surfaces
Zonal RANS-LES Computation for Near-Stall-Airfoil Flow
Criteria for Crosswind Variations during Approach and Touchdown at Airports
Development and Improvement of Two Methods of Different Complexity to Simulate Atmospheric Boundary Layer Turbulence for Aircraft Design Studies
Simulation of Interaction of Aircraft with Gust and Resolved LES-Simulated Atmospheric Turbulence
A New Method to Generate Anisotropic Synthetic Turbulence for LES
Numerical Simulation of the Turbulent Flow Around a Wing
Integration- and Intake-Induced Flow Distortions and their Impact on Aerodynamic Fan Performance
Flow Investigations in a Stalling Nacelle Inlet Under Disturbed Inflow
Realistic Inlet Distortion Patterns Interacting with a Transonic Compressor Stage
Unsteady CFD Simulation of Transonic Axial Compressor Stages with Distorted Inflow
Transitional Shock-Wave/Boundary-Layer Interactions in Intakes at Incidence.-Advanced Design Approach for a High-lift Wind Tunnel Model Based on Flight Test Data
Simulation of Longitudinal Vortices on a High-LiftWing
Impact of Different UHBR-Engine Positions on the Aerodynamics of a High-LiftWing
Numerical Investigation of the Influence of Pressure Belts on the Stall of a Transport Aircraft in Landing Configuration
Numerical Studies of Active Flow Control Applied at the Engine-Wing Junction.

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