Viscous Hypersonic Flow Past a Slender Cone-Reference-Cited by-同舟云学术

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Viscous Hypersonic Flow Past a Slender Cone

Published:1964 Issue:5 Volume:7 Page:667
ISSN:0031-9171
Container-title:Physics of Fluids
language:en
Short-container-title:Phys. Fluids

Author:

Stewartson K.

Publisher

AIP Publishing

Subject

General Engineering

Reference12 articles.

1. W. D. Hayes and R. F. Probstein,Hypersonic Flow Theory(Academic Press, Inc., New York, 1959).

2. K. Stewartson,Theory of Laminar Compressible Boundary Layers(Oxford University Press, London, 1964).

3. On the Hypersonic Viscous Flow Past Slender Bodies of Revolution

4. Axisymmetric Viscous Flow Past Very Slender Bodies of Revolution

Cited by 34 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. Unsteady hypersonic boundary layers for slender axisymmetric bodies with large injection rates;International Journal of Engineering Science;1992-06

2. Model for the Solution of Supersonic Viscous Interaction Effects on Blunted Cones;AIAA Journal;1975-03

3. DOWNSTREAM EFFECTS OF BLUNTNESS IN THE MERGED FLOW REGIME**This work was supported by the Air Force Office of Scientific Research under its contract F44620-71-C-0032 and by the National Science Foundation, NSF Grant GK-31204X.;Rarefied Gas Dynamics;1974

4. Multistructured Boundary Layers on Flat Plates and Related Bodies;Advances in Applied Mechanics;1974

5. Second approximation in the problem of the strong viscous interaction on slender three-dimensional bodies;Fluid Dynamics;1973

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