Secondary Instabilities in Supersonic Boundary Layers over Microporous Surfaces
Author:
Affiliation:
1. Ph.D. Candidate, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, China. ORCID: .
2. Professor, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, China (corresponding author). ORCID: .
Publisher
American Society of Civil Engineers (ASCE)
Subject
Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering
Link
https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-4816
Reference33 articles.
1. Oblique-mode breakdown and secondary instability in supersonic boundary layers
2. Fasel H. A. Thumm and H. Bestek. 1993. “Direct numerical simulation of transition in supersonic boundary layers: Oblique breakdown.” Transitional and turbulent compressible flows. In Vol. 151 of Proc. Fluids Engineering Division Conf. edited by L. D. Kral and T. A. Zang 77–92. New York: ASME.
3. Stabilization of Hypersonic Boundary Layers by Porous Coatings
4. Breakdown mechanisms and heat transfer overshoot in hypersonic zero pressure gradient boundary layers
5. RANS modeling of high-speed aerodynamic flow transition with consideration of stability theory
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