High-Order Implicit Large-Eddy Simulations of a Supersonic Corner Flow over a Compression Ramp
Author:
Affiliation:
1. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-3335
Reference55 articles.
1. Thermoacoustic loads and fatigue of hypersonic vehicle skin panels
2. Direct simulation of the turbulent boundary layer along a compression ramp at M = 3 and Reθ = 1685
3. Large-Eddy Simulation of Supersonic Compression-Ramp Flow by High-Order Method
4. Large Eddy Simulation of Shock/Boundary-Layer Interaction
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2. Comparison of Computational and Experimental Results in the Wake Region Behind a Wall-Mounted Hemisphere in Supersonic Flow;AIAA Aviation 2019 Forum;2019-06-15
3. Numerical Simulation of Sidewall Influence on Supersonic Compression Ramp Interactions;2018 Fluid Dynamics Conference;2018-06-24
4. Investigation of Shock-Boundary Layer Interaction Around Wall-Mounted Hemisphere using DDES and ILES;2018 AIAA Aerospace Sciences Meeting;2018-01-07
5. Supersonic Corner Flow Predictions using the Quadratic Constitutive Relation;22nd AIAA Computational Fluid Dynamics Conference;2015-06-18
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