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Hydromagnetic shock structure in high temperature hypersonic flow

✍ Scribed by A. R. Bestman


Publisher
Springer Netherlands
Year
1991
Tongue
English
Weight
381 KB
Volume
179
Category
Article
ISSN
0004-640X

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In the recent work of Prof. Hans Hornung, expressions for the gradients of flow properties immediately behind a curved shock wave were obtained for a reacting gas [1]. In this paper, I use the expressions derived by Hornung to compare with inviscid computational fluid dynamics simulations of a Mach