Performance of a supersonic ramp-type side inlet with ram-scoop throat bleed and varying fuselage boundary-layer removal : Mach number range 1.5 to 2.0

Author: Mitchell, Glenn A.
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E56I26
Link: https://digital.library.unt.edu/ark:/67531/metadc62848/

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