1. . Mechanics and Thermodynamics of Propulsion. Addison-Wesley Publishing Company: Reading, MA, 1992.
2. Supersonic Diffuser Instability
3. . Experimental investigation of a large-scale, two-dimensional, mixed-compression inlet system—performance at design conditions, m∞=3.0. Technical Report NASA TM X-2016, NASA Ames Research Center, 1970.
4. , . Design of a very-low-bleed mach 2.5 mixed-compression inlet with 45 percent internal contraction. Technical Report NASA TM X-3135, NASA, 1975.
5. Improved Calculation of High Speed Inlet Flows. Part II: Results