Investigation of the downwash and wake behind a triangular wing of aspect ratio 4 at subsonic and supersonic Mach numbers

Author: Walker, Harold J
Year: 1950
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A50I14a
Link: https://digital.library.unt.edu/ark:/67531/metadc58680/

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