Vor Ort
Merkzettel Warenkorb
  • Produktbild: Advances in Simulation of Wing and Nacelle Stall
  • Produktbild: Advances in Simulation of Wing and Nacelle Stall
Band 131 - 10%

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
10% sparen

191,99 € UVP 213,99 €

inkl. gesetzl. MwSt., Versandkostenfrei

Beschreibung

Produktdetails

Einband

Gebundene Ausgabe

Erscheinungsdatum

21.07.2015

Abbildungen

IX, 273 illus., 107 illus. in color., farbige Illustrationen, schwarz-weiss Illustrationen

Herausgeber

Rolf Radespiel + weitere

Verlag

Springer

Seitenzahl

413

Maße (L/B/H)

24,1/16/2,9 cm

Gewicht

799 g

Auflage

1st edition 2016

Sprache

Englisch

ISBN

978-3-319-21126-8

Beschreibung

Produktdetails

Einband

Gebundene Ausgabe

Erscheinungsdatum

21.07.2015

Abbildungen

IX, 273 illus., 107 illus. in color., farbige Illustrationen, schwarz-weiss Illustrationen

Herausgeber

Verlag

Springer

Seitenzahl

413

Maße (L/B/H)

24,1/16/2,9 cm

Gewicht

799 g

Auflage

1st edition 2016

Sprache

Englisch

ISBN

978-3-319-21126-8

Herstelleradresse

Springer-Verlag KG
Sachsenplatz 4-6
1201 Wien
AT

Email: GPSR Kontakt

Noch keine Bewertungen vorhanden

Verfassen Sie die erste Bewertung zu diesem Artikel

Helfen Sie anderen Kundinnen und Kunden durch Ihre Meinung.

Kundinnen und Kunden meinen

Bewertungen (0)
Die Leseprobe wird geladen.
  • 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.