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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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