Experimental investigation of supersonic flow with detached shock waves for Mach numbers between 1.8 and 2.9

Author:	Moeckel, W E
Year:	1950
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E50D05
Link:	https://digital.library.unt.edu/ark:/67531/metadc58461/