Stability of thin Viscous Shock Layer on a Wedge in Hypersonic Flow of a Perfect Gas-Reference-Cited by-同舟云学术

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Stability of thin Viscous Shock Layer on a Wedge in Hypersonic Flow of a Perfect Gas

Published:1985 Issue: Volume: Page:487-493
ISSN:
Container-title:Laminar-Turbulent Transition
language:
Short-container-title:

Author:

Petrov G. V.

Publisher

Springer Berlin Heidelberg

Link

http://link.springer.com/content/pdf/10.1007/978-3-642-82462-3_59.pdf

Reference4 articles.

1. Hayes, W.D.; Probstein, R.F.: Hypersonic flow theory. Second ed., vol. 1, Inviscid flow. N.-Y, London: Academic press 1966.

2. Mack, L.M.: Boundary layer stability theory. Doc. 900–277, Rev. A. Pasadena: JPL 1969.

3. Dunn, D.W.; Lin, C.C.: On the stability of the laminar boundary layer in a compressible fluid. J. Aeron. Sci. 22, N 7 (1969).

4. De Bruijn, N.G.: Asymptotic methods in analysis. Amsterdam, Groningen 1958.

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. Numerical simulation of receptivity of a hypersonic boundary layer to acoustic disturbances;Journal of Applied Mechanics and Technical Physics;2007-05

2. Hypersonic Shear Layer Stability Experiments;Journal of Spacecraft and Rockets;2005-11

3. Mode switching in a supersonic boundary layer;Journal of Applied Mechanics and Technical Physics;1993

4. Asymptotic structure of inviscid disturbances in a thin shock layer;Fluid Dynamics;1989

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