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Singularities of attached shock waves in steady axially symmetric flow
Published online by Cambridge University Press: 28 March 2006
Abstract
An I.B.M. 704 electronic computer was used to integrate the differential equations, which determine the shock singularity, when the velocity after the shock on a body is subsonic. The results are given in twenty-two cases corresponding to three different bodies; the procedure followed was outlined in a previous paper (Cabannes 1952).
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- © 1961 Cambridge University Press
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