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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

Aus der Reihe Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Beschreibung

Produktdetails

Einband

Gebundene Ausgabe

Erscheinungsdatum

21.07.2015

Abbildungen

IX, 413 p. 273 illus., 107 illus. in color.

Herausgeber

Rolf Radespiel + weitere

Verlag

Springer

Seitenzahl

413

Maße (L/B/H)

24,1/16/2,9 cm

Gewicht

799 g

Auflage

1st ed. 2016

Sprache

Englisch

ISBN

978-3-319-21126-8

Beschreibung

Produktdetails

Einband

Gebundene Ausgabe

Erscheinungsdatum

21.07.2015

Abbildungen

IX, 413 p. 273 illus., 107 illus. in color.

Herausgeber

Verlag

Springer

Seitenzahl

413

Maße (L/B/H)

24,1/16/2,9 cm

Gewicht

799 g

Auflage

1st ed. 2016

Sprache

Englisch

ISBN

978-3-319-21126-8

Herstelleradresse

Springer-Verlag KG
Sachsenplatz 4-6
1201 Wien
AT

Email: ProductSafety@springernature.com

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  • Produktbild: Advances in Simulation of Wing and Nacelle Stall
  • Produktbild: Advances in Simulation of Wing and Nacelle Stall

  • 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.