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Force and pressure recovery characteristics at supersonic speeds of a conical spike inlet with a bypass discharging from the top or bottom of the diffuser in an axial direction
Author:
Allen, J. L.
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E53A29
Link:
https://digital.library.unt.edu/ark:/67531/metadc59602/
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