Effect of tip vortex structure on helicopter noise due to...

Journal of Aircraft 1980 / 10 Vol. 17; Iss. 10

Effect of tip vortex structure on helicopter noise due to blade-vortex interaction

WIDNALL, S. E., WOLF, T. L.
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Volume:
17
Language:
english
Journal:
Journal of Aircraft
DOI:
10.2514/3.44681
Date:
October, 1980
File:
PDF, 824 KB
english, 1980
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