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

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/

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