Abstract
A wedge with a thin plate in front of it has an angle of 16° and is subjected to a plane supersonic flow of an ideal gas (γ = 1.4). The approach flow is parallel to the plate such that the plate’s leading edge causes only a small perturbation (Mach wave).
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© 1997 Springer-Verlag Berlin Heidelberg
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Spurk, J.H. (1997). Supersonic Flow. In: Fluid Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-58277-6_11
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DOI: https://doi.org/10.1007/978-3-642-58277-6_11
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-63523-6
Online ISBN: 978-3-642-58277-6
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