1. Supersonic vehicle systems for the 2020 to 2035 timeframe;Nelson,2010
2. Pressure recovery for missiles with reaction propulsion at high supersonic speeds (The efficiency of shock diffusers), NACA-TM-1140;Oswatitsch,1947
3. Microramp control of supersonic oblique shock-wave/boundary-layer interactions;Babinsky;AIAA J.,2009
4. Control of supersonic inlet-isolator unstart using active and passive vortex generators;Valdivia;AIAA J.,2014
5. Performance of a supersonic ramp-type side inlet with ramp-scoop throat and varying fuselage boundary-layer removal Mach number range 1.5 to 2.0, NACA-RM-E56I26;Mitchell,1957