Force and pressure recovery characteristics at supersonic speeds of a conical spike inlet with a bypass discharging from the top or bottom of the diffuser in an axial direction

Author: Allen, J. L.
Year: 1953
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E53A29
Link: https://digital.library.unt.edu/ark:/67531/metadc59602/

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