Low-speed pressure-distribution and flow investigation for a large pitch and yaw range of three low-aspect-ratio pointed wings having leading edge swept back 60 degrees and biconvex sections

Author: May, Ralph W., Jr.
Year: 1949
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L9J07
Link: https://digital.library.unt.edu/ark:/67531/metadc58372/

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