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| 2000-2001 Fluids Seminar Page |
School of Aerospace Engineering
Ryerson Polytechnic University
350 Victoria Street
Toronto, Ontario M5B 2K3
Canada
Abstract-
A brief description is given of the derivation of the first order
gradient equations of doubly curved shock waves for non-uniform flow
of a perfect gas. These equations are then applied to a series of
simple and not-so-simple curved shock configurations. The potentially
outrageous behaviour of three coalescing shock waves is exposed.
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