1. Maurer, F., Brungs, W.: Beeinflussung des Widerstands und der Kopfwelle durch Wärmezufuhr im Staupunktsbereich stumpfer Körper bei Überschallanströmung, Jahrbuch 1968 der DGLR, Köln (in German), pp. 174–189 (1968)
2. Maurer, F., Brungs, W.: Shockwave and drag variation of blunt bodies in supersonic flow by heat addition in the stagnation point region. Boeing Translation Nr. B-803
3. Reding, J.P., Jecmen, D.M.: Effects of external burning on spike-induced separated flow. J. Spacecraft Rockets, 20(5), 452–453 (1983); also AIAA-82-1360 (1982)
4. Baev, V.K., Golovichev, V.I., Tretyakov, P.K., et al.: Combustion in Supersonic Flow (in Russian). Nauka, Novosibirsk (1984)
5. Zubkov A.I., Garanin A.F., Safronov V.F., Sukhanoskaya L.D., Tretyakov P.K.: Supersonic flow past an axisymmetric body with combustion in separation zones at the body nose and base (in Russian). Thermoph. Aeromech. 12(1), 1–12 (2005)