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Effects of compressibility, pitch rate, and Reynolds number on unsteady incipient leading-edge boundary layer separation over a pitching airfoil

✍ Scribed by Choudhuri, P. Ghosh; Knight, D. D.

Book ID: 120138341
Publisher: Cambridge University Press
Year: 1996
Tongue: English
Weight: 523 KB
Volume: 308
Category: Article
ISSN: 0022-1120
DOI: 10.1017/S0022112096001450

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