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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