Preliminary investigation of effect of angle of attack on pressure recovery and stability characteristics for a vertical-wedge-nose inlet at Mach number of 1.90

Author:	Leissler, L. Abbott
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E52E14
Link:	https://digital.library.unt.edu/ark:/67531/metadc59242/