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DTIC ADA367319: An Experimental Investigation of Tangential Blowing to Reduce Buffet Response of the Vertical Tails of an F-15 Wind Tunnel Model. Volume 1. Tests Results, Discussion and Correlation. PDF

241 Pages·6.3 MB·English
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by Defense Technical Information Center| 241 pages| 6.3| English

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Author:Defense Technical Information Center
Pages:241
Language:English
File Size:6.3
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