Hypersonic Flow Past a Wedge at Small Angles of Attack
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Authors
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Department of Mathematics, Science College, Patna 5 ,IN
Girishwar Nath
DOI:
https://doi.org/10.18311/jims/1965/16821Abstract
A closed form solution to the inviscid hypersonic inotational flow over a wedge, at small angles of attack, with an attached shock wave is considered here. Viscosity, heat transfer and skin-friction etc. have been completely neglected.
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Published
1965-06-01
How to Cite
Nath, G. (1965). Hypersonic Flow Past a Wedge at Small Angles of Attack. The Journal of the Indian Mathematical Society, 29(1-2), 37–48. https://doi.org/10.18311/jims/1965/16821
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Copyright (c) 1965 Girishwar Nath
This work is licensed under a Creative Commons Attribution 4.0 International License.
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