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Shock waves in a dusty gas

Published online by Cambridge University Press:  28 March 2006

G. F. Carrier
G. F. Carrier
Affiliation:
Pierce Hall, Harvard University
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Abstract

The plane steady decelerated flow of a dust-gas mixture is analysed in an approximate manner. The problem, which has a five-parameter family of solutions, is reduced to a form such that the analysis can be completed by the integration of a first-order non-linear differential equation and a quadrature. A few integral curves are given and the characterizing features of the flow field are discussed.

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 4 , Issue 4 , August 1958 , pp. 376 - 382
Copyright
© Cambridge University Press

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