1. Oswatitsch K (1947) Pressure recovery in missiles with reaction propulsion at high supersonic speeds. National Advisory Committee for Aeronautics Technical Memorandum No. 1140, June 1947
2. Anderson JD (1997) A history of aerodynamics and its impact on flying machines. Cambridge University Press, Cambridge
3. Conners JS, Meyer RC (1956) Design criteria for axisymmetric and two-dimensional supersonic inlets and exits. National Advisory Committee for Aeronautics Technical Note 3589, Jan 1956
4. Trexler CA (1974) Performance of an inlet for an intergraded scramjet concept. J Aircraft 11(9):589–591
5. Trexler CA (1988) Inlet starting prediction for sidewall compression-scramjet inlets. In: 24th Joint Propulsion Conference, Boston, MA, USA, 11–13 July 1988