Direct Numerical Simulation of Shockwave and Turbulent Boundary Layer Interactions
Author:
Affiliation:
1. Princeton University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-589
Reference29 articles.
1. Direct Numerical Simulation of Supersonic Turbulent Boundary Layer over a Compression Ramp
2. Large Eddy Simulation of Shock/Boundary-Layer Interaction
3. Oblique Shock Impinging on a Turbulent Boundary Layer: Low-Frequency Mechanisms.
4. Direct simulation of the turbulent boundary layer along a compression ramp at M = 3 and Reθ = 1685
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2. Delayed Detached Eddy Simulation of Supersonic Panel Aeroelasticity Using Fully Coupled Fluid Structure Interaction with High Order Schemes;34th AIAA Applied Aerodynamics Conference;2016-06-10
3. Prediction of Wing Flutter Boundary Using High Fidelity Delayed Detached Eddy Simulation;56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2015-01-02
4. DNS of a Spatially Evolving Transitional/Turbulent Boundary Layer with Impinging Shock Wave;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
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