A Preliminary Investigation of the Pressure Recovery of Several Two-Dimensional Supersonic Inlets at Mach Number of 2.01

Author: Comenzo, Raymond J.
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L54D14
Link: https://digital.library.unt.edu/ark:/67531/metadc60464/

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