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

Author:	Katzen, Elliott D.
Additional Authors:	Frick, Charles W.
Year:	1948
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A8F22
Link:	https://digital.library.unt.edu/ark:/67531/metadc57778/