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Influence of the sweepback angle and the unit reynolds number on boundary-layer transition at supersonic velocities

โœ Scribed by S. V. Kalinina; V. I. Kornilov


Publisher
SP MAIK Nauka/Interperiodica
Year
1975
Tongue
English
Weight
251 KB
Volume
14
Category
Article
ISSN
0021-8944

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