Experimental and numerical investigation of development of disturbances in the boundary layer on sharp and blunted cone
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Reference28 articles.
1. J.J. Bertin. Hypersonic Aerothermodynamics (AIAA, Washington, DC, 1994).
2. Linear Stability Theory and the Problem of Supersonic Boundary- Layer Transition
3. J.J. White. Viscous Fluid Flow (McGraw-Hill, New York, 1974).
4. Prediction and control of transition in supersonic and hypersonic boundary layers
5. G. Gasperas, “The stability of the compressible boundary layer on a sharp cone at zero angle of attack”, AIAA Paper No. 87-0494 (1987).
Cited by 4 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. Flow structures in transitional and turbulent boundary layers;Physics of Fluids;2019-11-01
2. Numerical Study of the Evolution of Disturbances Generated by Roughness Elements in a Supersonic Boundary Layer on a Blunted Cone;Journal of Applied Mechanics and Technical Physics;2019-05
3. Numerical study of surface roughness effects in the boundary layer of a blunted cone in a supersonic flow;AIP Conference Proceedings;2018
4. Experimental investigation of the hypersonic boundary layer transition on a 7° straight cone;Acta Physica Sinica;2018
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