A solution for hypersonic flow past slender bodies-Reference-Cited by-同舟云学术

A solution for hypersonic flow past slender bodies

Published:1971-07-13 Issue:1 Volume:48 Page:23-31
ISSN:0022-1120
Container-title:Journal of Fluid Mechanics
language:en
Short-container-title:J. Fluid Mech.

Author:

Hui W. H.

Abstract

A solution to the hypersonic small disturbance equations is obtained for a class of two-dimensional bodies supporting logarithmic shock waves by reducing the partial differential equation to an ordinary differential equation. The body shape is calculated and shown not to be logarithmic if γ ≠ 1, where γ is the ratio of the specific heats of the gas.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference3 articles.

1. Cole, J. D. & Aroesty, J. 1970 Hypersonic similarity solutions for airfoils supporting exponential shock waves A.I.A.A. J. 8,308.

2. Sedov, L. I. 1959 Similarity and Dimensional Methods in Mechanics ,4th edition, ch. iv. (English transl.ed. M. Holt .)Academic.

3. Mirels, H. 1962 Hypersonic flow over slender bodies associated with power law shocks. Advances in Applied Mechanics , vol. vii.

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