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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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