Investigation of the air-flow-regulation characteristics of a translating-spike inlet with two oblique shocks from Mach 1.6 to 2.0

Author: Nettles, J. C.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E56D23B
Link: https://digital.library.unt.edu/ark:/67531/metadc53048/

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