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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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