Axisymmetric hypersonic flow with strong viscous interaction-Reference-Cited by-同舟云学术

Axisymmetric hypersonic flow with strong viscous interaction

Published:1968-12-23 Issue:4 Volume:34 Page:687-703
ISSN:0022-1120
Container-title:Journal of Fluid Mechanics
language:en
Short-container-title:J. Fluid Mech.

Author:

Ellinwood John Webster,Mirels Harold

Abstract

Stewartson's theory for axisymmetric hypersonic flow of a model gas over slender bodies with strong viscous interaction and strong shock wave is extended to power-law viscosity variation and Prandtl numbers other than one. Flow properties at the body surface and shock are obtained without recourse to numerical integration. Numerical computations are presented for axisymmetric flow over a three-quarter power-law body with strong shock wave and viscous interactions that range from weak to strong.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference13 articles.

1. Stewartson, K. 1955 Quart. Appl. Math. 13,113.

2. Bush, W. B. 1966 J. Fluid Mech. 25,51.

3. Yasuhara, M. 1956 J. Phys. Soc. Japan,11,878.

4. Moore, F. K. 1952 Nat. Adv. Comm. Aero. Tech. Note, NACA TN 2722.

5. Stewartson, K. 1964 Phys. Fluids, 7, 667;7,2025.

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