Hypersonic flow past a wing at large angles of attack with...

Fluid Dynamics 1985 / 05-06 Vol. 20; Iss. 3

Hypersonic flow past a wing at large angles of attack with detached shock wave

V. N. Golubkin, V. V. Negoda
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Volume:
20
Language:
english
Pages:
8
DOI:
10.1007/bf01050004
Date:
May, 1985
File:
PDF, 664 KB
english, 1985
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