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Advances in Simulation of Wing and Nacelle Stall

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Cover of 'Advances in Simulation of Wing and Nacelle Stall'

Table of Contents

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    Book Overview
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    Chapter 1 The Delay of RANS-to-LES Transition in Hybrid RANS-LES Approaches and Some Recently Proposed Remedies
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    Chapter 2 Computations of Separated Flows with a Hybrid RANS/LES Approach
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    Chapter 3 Hybrid RANS/LES Study of the Development of an Airfoil-Generated Vortex
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    Chapter 4 Interaction of Three-Dimensional Disturbances with the Flow Around a Two-Element High-Lift Airfoil
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    Chapter 5 The Discontinuous Galerkin Method as an Enabling Technology for DNS and LES of Industrial Aeronautical Applications
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    Chapter 6 Advances in Simulation of Wing and Nacelle Stall
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    Chapter 7 Numerical Studies of Turbulent Flow Influence on a Two-Element Airfoil
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    Chapter 8 CFD for Prediction of Flow Separation from Aircraft Tail Surfaces
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    Chapter 9 Zonal RANS-LES Computation for Near-Stall-Airfoil Flow
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    Chapter 10 Criteria for Crosswind Variations during Approach and Touchdown at Airports
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    Chapter 11 Development and Improvement of Two Methods of Different Complexity to Simulate Atmospheric Boundary Layer Turbulence for Aircraft Design Studies
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    Chapter 12 Simulation of Interaction of Aircraft with Gust and Resolved LES-Simulated Atmospheric Turbulence
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    Chapter 13 A New Method to Generate Anisotropic Synthetic Turbulence for LES
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    Chapter 14 Numerical Simulation of the Turbulent Flow Around a Wing
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    Chapter 15 Integration- and Intake-Induced Flow Distortions and Their Impact on Aerodynamic Fan Performance
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    Chapter 16 Flow Investigations in a Stalling Nacelle Inlet Under Disturbed Inflow
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    Chapter 17 Realistic Inlet Distortion Patterns Interacting with a Transonic Compressor Stage
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    Chapter 18 Unsteady CFD Simulation of Transonic Axial Compressor Stages with Distorted Inflow
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    Chapter 19 Advances in Simulation of Wing and Nacelle Stall
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    Chapter 20 Advanced Design Approach for a High-Lift Wind Tunnel Model Based on Flight Test Data
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    Chapter 21 Simulation of Longitudinal Vortices on a High-Lift Wing
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    Chapter 22 Impact of Different UHBR-Engine Positions on the Aerodynamics of a High-Lift Wing
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    Chapter 23 Numerical Investigation of the Influence of Pressure Belts on the Stall of a Transport Aircraft in Landing Configuration
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    Chapter 24 Numerical Studies of Active Flow Control Applied at the Engine-Wing Junction
Attention for Chapter 5: The Discontinuous Galerkin Method as an Enabling Technology for DNS and LES of Industrial Aeronautical Applications
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Chapter title
The Discontinuous Galerkin Method as an Enabling Technology for DNS and LES of Industrial Aeronautical Applications
Chapter number 5
Book title
Advances in Simulation of Wing and Nacelle Stall
Published by
Springer, Cham, January 2016
DOI 10.1007/978-3-319-21127-5_5
Book ISBNs
978-3-31-921126-8, 978-3-31-921127-5
Authors

Koen Hillewaert, Corentin Carton de Wiart, Hillewaert, Koen, Carton de Wiart, Corentin, Wiart, Corentin Carton de, de Wiart, Corentin Carton

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X Demographics

The data shown below were collected from the profile of 1 X user who shared this research output. Click here to find out more about how the information was compiled.
Mendeley readers

Mendeley readers

The data shown below were compiled from readership statistics for 2 Mendeley readers of this research output. Click here to see the associated Mendeley record.

Geographical breakdown

Country Count As %
Unknown 2 100%

Demographic breakdown

Readers by professional status Count As %
Student > Postgraduate 1 50%
Unknown 1 50%
Readers by discipline Count As %
Engineering 1 50%
Unknown 1 50%