Double Peak-Heating in Hypersonic Transitional Shock-Wave/Boundary-Layer Interactions
Author:
Affiliation:
1. National Cheng Kung University, Tainan City 701, Taiwan, Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061094
Reference22 articles.
1. Shock Wave–Boundary-Layer Interactions
2. HirschelE.ClausW., Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles, Vol. 229, Springer Science & Business Media, Berlin, 2009, pp. 13–37, Chap. 2.1.
3. Aerothermodynamics – A critical review at DLR
4. Hypersonic shock wave transitional boundary layer interactions - A review
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