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
1956
34 pages
Report
No indication
English
Boundary layer control , Fuselage , Ramp , Side inlet , Boundary , Control , Fairing , Flush , Inlet , Internal , Layer , Perforation , Side , Slot , Speed , Stability , Supersonic , Throat