Aerodynamic characteristics at Mach numbers 2.36 and 2.87 of an airplane configuration having a cambered arrow wing with a 75 degree swept leading edge

Author:	Hallissy, Joseph M., Jr.
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L58E21
Link:	https://digital.library.unt.edu/ark:/67531/metadc64269/