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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 /

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 n...

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Corporate Author: SpringerLink (Online service)
Other Authors: Radespiel, Rolf. (Editor, http://id.loc.gov/vocabulary/relators/edt), Niehuis, Reinhard. (Editor, http://id.loc.gov/vocabulary/relators/edt), Kroll, Norbert. (Editor, http://id.loc.gov/vocabulary/relators/edt), Behrends, Kathrin. (Editor, http://id.loc.gov/vocabulary/relators/edt)
Language:English
Published: Cham : Springer International Publishing : Imprint: Springer, 2016.
Edition:1st ed. 2016.
Series:Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 131
Subjects:
Fluid mechanics.
Fluids.
Aerospace engineering.
Astronautics.
Engineering Fluid Dynamics.
Fluid- and Aerodynamics.
Aerospace Technology and Astronautics.
Online Access:https://doi.org/10.1007/978-3-319-21127-5
Table of Contents:
  • 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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