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Author:Defense Technical Information Center
Language:English
File size:6.3 MB
Number of page:241
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Similar 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.

Most books are stored in the elastic cloud where traffic is expensive. For this reason, we have a limit on daily download.