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The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75
Author:
Burbank, Paige B.
Year:
1953
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-2921
Link:
https://digital.library.unt.edu/ark:/67531/metadc56660/
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