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Effect of fuselage circumferential inlet location on diffuser-discharge total-pressure profiles at supersonic speeds
Author:
Kremzier, Emil J
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E56G26
Link:
https://digital.library.unt.edu/ark:/67531/metadc64441/
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