Effects of Parallel-Jet Mixing on Downstream Mach Number and Stagnation Pressure With Application to Engine Testing in Supersonic Tunnels

Document details
Author:	Bernstein, Harry
Year:	1953
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2918
Link:	https://digital.library.unt.edu/ark:/67531/metadc56646/