Investigation at supersonic speed (M = 1.53) of the pressure distribution over a 63 degrees swept airfoil of biconvex section at zero lift

Author: Boyd, John W
Year: 1948
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A8C22
Link: https://digital.library.unt.edu/ark:/67531/metadc57586/

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