Pressure Recovery for Missiles with Reaction Propulsion at High Supersonic Speeds (The Efficiency of Shock Diffusers)

Author:	Oswatitsch, K.
Year:	1947
Document Type:	N/A
Series:	NACA Technical Memorandums
Report Number:	NACA-TM-1140
Link:	https://digital.library.unt.edu/ark:/67531/metadc63721/