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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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