Experimental Pressure Distributions Over Wing Tips at Mach Number 1.9 1 - Wing Tip With Subsonic Leading Edge

Author:	Jagger, James M.
Year:	1949
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E8K26
Link:	https://digital.library.unt.edu/ark:/67531/metadc57955/