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RecordNumber
4519
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Title
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
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Author Statement
edited by Rolf Radespiel, Reinhard Niehuis, Norbert Kroll, Kathrin Behrends
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Edition
1st ed. 2016.
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Collation
1 online resource (IX, 413 pages 273 illustrations, 107 illustrations in color.)
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Series
Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Notes
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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Subject
Fluid mechanics. , Fluids. , Aerospace engineering. , Astronautics. , Engineering Fluid Dynamics. , Fluid- and Aerodynamics. , Aerospace Technology and Astronautics.
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ADDED ENTRIES
Radespiel, Rolf. , Niehuis, Reinhard. , Kroll, Norbert. , Behrends, Kathrin.
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