Investigation of translating-spike supersonic inlet as means of mass-flow control at Mach numbers of 1.5, 1.8, and 2.0

Author: Gorton, Gerald C.
Year: 1953
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E53G10
Link: https://digital.library.unt.edu/ark:/67531/metadc59636/

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