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The ShockWave Cubic

The ShockWave Cubic The inverse problem of finding the shockwave angle when a supersonic stream passes round a bend of 180i involves a double interpolation from tables prepared for the direct problem. This may be avoided by reducing the problem to the solution of a cubic equation. Most of the phenomena associated with oblique shock waves can be deduced from this cubic equation. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

The ShockWave Cubic

Naylor, V.D.
Aircraft Engineering and Aerospace Technology , Volume 26 (12): 3 – Dec 1, 1954
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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb032501
Publisher site
See Article on Publisher Site

Abstract

The inverse problem of finding the shockwave angle when a supersonic stream passes round a bend of 180i involves a double interpolation from tables prepared for the direct problem. This may be avoided by reducing the problem to the solution of a cubic equation. Most of the phenomena associated with oblique shock waves can be deduced from this cubic equation.

Journal

Aircraft Engineering and Aerospace Technology – Emerald Publishing

Published: Dec 1, 1954

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