Curvature of attached shock waves in steady axially symmetric flow-Reference-Cited by-同舟云学术

Curvature of attached shock waves in steady axially symmetric flow

Published:1960-04 Issue:4 Volume:7 Page:610-616
ISSN:0022-1120
Container-title:Journal of Fluid Mechanics
language:en
Short-container-title:J. Fluid Mech.

Author:

Bianco E.,Cabannes H.,Kuntzmann J.

Abstract

An electronic computer has been employed to calculate the ratio between the initial radii of curvature of the attached shock wave and the body for an axially symmetrical body in a uniform supersonic stream. The results are obtained with 4 exact digits for more than 200 cases. They extend results obtained previously (Cabannes 1951) by means of numerical integration.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference4 articles.

1. Shen, S. F. & Lin, C. C. 1951 On the attached curved shock in front of a sharp-nosed axially symmetrical body placed in a uniform stream.N.A.C.A. Technical Note, 2505.

2. Kopal, Zdenek 1947 Tables of supersonic flow around cones .Massachusetts Institute of Technology.

3. Cabannes, H. 1951 Etude de l'onde de choc attachée dans les écoulements de révolution.Rech. aéro.,24,17–23.

4. Rao, P. S. 1956 Supersonic bangs.Aeronaut. Quart.,7,135–55.

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