Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99 III : conical-spike all-external-compression inlet with supersonic cowl lip

Author: Weinstein, Maynard I
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E50J30
Link: https://digital.library.unt.edu/ark:/67531/metadc58637/

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