1. Pressure recovery for missiles with reaction propulsion at high supersonic speeds;Oswatitsch,1947
2. The origin of aerodynamic instability of supersonic inlet at subcritical condition;Ferri,1951
3. Supersonic diffuser instability;Dailey,1954
4. On the subcritical stability of variable ramp intakes at Mach number around 2.0;Fisher,1970
5. External-compression supersonic inlet free from violent buzz;Chen;AIAA J.,2019