Performance of a Double-Ramp Side Inlet With Combinations of Fuselage, Ramp, and Throat Boundary-Layer Removal, Mach Number Range, 1.5 to 2.0

Author: Simon, Paul C.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E56G09A
Link: https://digital.library.unt.edu/ark:/67531/metadc52965/

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