Investigation of Pressure Recovery of a Single-Conical-Shock Nose Inlet at Mach Number 5.4

Author: Bernstein, Harry
Year: 1953
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E53A12
Link: https://digital.library.unt.edu/ark:/67531/metadc59532/

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