1. AIAA Progress in Astronautics and Aeronautics;Anderson G.Y.,2000
2. Ramjet Nozzle Analysis for Transport Aircraft Configuration for Sustained Hypersonic Flight
3. Baker N.R. Northam G.B. Stouffer S.D. andCapriotti D.P.(1993).Evaluation of scramjet nozzle configurations and film cooling for reduction of wall heating.AIAA Paper 93‐0744. 31st Aerospace Sciences Meeting Reno NV(11–14 January 1993).
4. Thrust augmentation through after-burning in scramjet nozzles
5. Deere K.A.andAsbury S.C.(1999).Experimental and computational investigation of a translating‐throat single‐expansion‐ramp nozzle. NASA/TP‐1999‐209138. NASA LaRC (May 1999).