Advances in Simulation of Wing and Nacelle Stall - Bookswagon
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Advances in Simulation of Wing and Nacelle Stall

Advances in Simulation of Wing and Nacelle Stall


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International Edition


About the Book

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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Product Details
  • ISBN-13: 9783319370675
  • Publisher: Springer
  • Publisher Imprint: Springer
  • Edition: Softcover reprint of the original 1st ed. 2016
  • Language: English
  • Returnable: Y
  • Spine Width: 22 mm
  • Weight: 643 gr
  • ISBN-10: 3319370677
  • Publisher Date: 15 Oct 2016
  • Binding: Paperback
  • Height: 234 mm
  • No of Pages: 413
  • Series Title: Notes on Numerical Fluid Mechanics and Multidisciplinary Des
  • Sub Title: Results of the Closing Symposium of the Dfg Research Unit for 1066, December 1-2, 2014, Braunschweig, Germany
  • Width: 156 mm


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