Effect of Two-Dimensional Short Rectangular Indentations on Hypersonic Boundary-Layer Transition
Author:
Affiliation:
1. Tianjin University, Tianjin 300072, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J059957
Reference45 articles.
1. Review of numerical simulations for high-speed, turbulent cavity flows
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4. Effects of Cavities and Protuberances on Transition over Hypersonic Vehicles
5. Study on Hypersonic Flow over Flat Plate with Channels
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