Performance of Twin-Duct Variable-Geometry Side Inlets at Mach Numbers of 1.5 to 2.0
1957
31 pages
Report
No indication
English
Aerodynamics , Air duct , Supersonic wind tunnel , Variable geometry structure , Air , Canard , Duct , Fuselage , Geometry , Inlet , Oscillation , Ramp , Shock , Structure , Supersonic , Tunnel , Variable , Wind