1. 2Park, H-K. "Model of an Aero-Space Plane Based on an Idealized Cone-Derived Waverider Forebody," Ph.D. Dissertation,University of Oklahoma, 1990.
2. Flows with heat addition
3. 4Sutton, G. P., Rocket Propulsion Elements, Secondedition,J. Wiley, NewYork, 1956, pp.30-34.
4. 5ANSER, NPO Energomash, Center for International Aerospace Cooperation, Arlington, VA, 1996,pp.2-9to 2-11.