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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