Investigation of a Half-Conical Scoop Inlet Mounted at Five Alternate Circumferential Locations Around a Circular Fuselage: Pressure-Recovery Results at a Mach Number 2.01

Author: Hasel, Lowell E.
Additional Authors: Lankford, John L.
Year: 1953
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L53D30B
Link: https://digital.library.unt.edu/ark:/67531/metadc64317/

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