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A new method for treating supersonic flow past nearly plane wings

✍ Scribed by Lewin, Myrna; Schmeltzer, Robert A.


Book ID
120113757
Publisher
Cambridge University Press
Year
1963
Tongue
English
Weight
177 KB
Volume
17
Category
Article
ISSN
0022-1120

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Direct problem and inverse problem for t
✍ Libin Wang πŸ“‚ Article πŸ“… 2011 πŸ› John Wiley and Sons 🌐 English βš– 175 KB

In this paper, we consider the isentropic irrotational steady plane flow past a curved wedge. First, for a uniform supersonic oncoming flow, we study the direct problem: For a given curved wedge y D f .x/, how to globally determine the corresponding shock y D g.x/ and the solution behind the shock?