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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