Simulations of Supersonic Flow over a Wall-Mounted Cylinder Using OVERFLOW with ILES
Author:
Affiliation:
1. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3956
Reference19 articles.
1. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
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2. Effect of Submergence on the Flow Around a Canonical Hemisphere at Transonic Conditions;AIAA SCITECH 2022 Forum;2022-01-03
3. 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
4. Comparison of Computational and Experimental Results on a Transonic Hemisphere;AIAA Scitech 2019 Forum;2019-01-06
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