Selective enhancement of oblique waves caused by finite amplitude second mode in supersonic boundary layer
Author:
Publisher
Springer Science and Business Media LLC
Subject
Applied Mathematics,Mechanical Engineering,Mechanics of Materials
Link
http://link.springer.com/article/10.1007/s10483-017-2227-9/fulltext.html
Reference26 articles.
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3. Kachanov, Y. S. Physical mechanisms of laminar-boundary-layer transition. Annual Review of Fluid Mechanics, 26(1), 411–482 (1994)
4. Li, X., Fu, D., and Ma, Y. Direct numerical simulation of hypersonic boundary layer transition over a blunt cone. AIAA Journal, 46(11), 2899–2913 (2008)
5. Li, X., Fu, D., and Ma, Y. Direct numerical simulation of hypersonic boundary layer transition over a blunt cone with a small angle of attack. Physics of Fluids (1994–present), 22(2), 025105 (2010)
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