The Role of Boundary-Layer Thickness on Cylinder-Generated Shock-Wave/Turbulent Boundary-Layer Interactions, Part I: Computations
Author:
Affiliation:
1. University of Tennessee, Tullahoma
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0380
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1. Separated Shock-Boundary-Layer Interaction Control Using Streamwise Slots
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Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Simulations of Dynamic Shock Wave/Boundary Layer Interactions Using HPCMP CREATETM-AV Kestrel COFFE;AIAA Scitech 2021 Forum;2021-01-04
2. The Role of Boundary-Layer Thickness on Cylinder-Generated Shock-Wave/Turbulent Boundary-Layer Interactions, Part II: Experiments;2018 AIAA Aerospace Sciences Meeting;2018-01-07
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