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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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