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Some Effects of Sweep and Thickness on the Experimental Downwash Characteristics at Transonic Speeds of a Series of Highly Tapered Wings With an Aspect Ratio of 3: Transonic Bump Method
Author:
Few, Albert G., Jr.
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L55J12
Link:
https://digital.library.unt.edu/ark:/67531/metadc61983/
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