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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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