N. U. Bakirov, “Convective heat transfer in convergent and divergent axisymmetric nozzles,” Izv. VUZ. Aviatsionnaya Tekhnika, no. 4, 1958.
O. A. Saunders and P. H. Calder, ldHeat transfer in nozzles at supersonic speeds,” Eng., August, no. 8, 1952.
W. E. Welsh and A. B. Witte, “Comparison of local heat fluxes found theoretically and experimentally in the chambers of liquid rocket motors,” Teploperedacha [Russian translation], no. 1, 1962.
A. B. Witte and E. H. Harper, “Experimental investigation of heat transfer in rocket motor nozzles,” Raketnaya tekhnika i kosmonavtika [Russian translation], no. 2, 1963.
S. Greenfield, “Determination of rocket motor heat transfer coefficients by the transient method,” J. Amer. Scien., vol. 18, no. 8, 1951.
D. R. Bartz, “An approximate solution of compressible turbulent boundary layer development and convective heat transfer in convergent-divergent nozzles,” Trans. ASME, vol. 77, no. 8, 1955.
D. R. Bartz, “A simple equation for rapid estimation of rocket nozzle convective heat transfer coefficients,” J. Jet Propuls., no. 1, 1957.
E. U. Repik and V. E. Chekalin, “Convective heat transfer in supersonic nozzles,” Inzh. zh., vol. 2, no. 2, 1962.
S. S. Kutateladze and A. I. Leont'ev, Turbulent Boundary Layer of a Compressible Gas [in Russian], Izd. SO AN SSSR, 1962.
Collection: Friction and Heat and Mass Transfer in a Turbulent Boundary Layer [in Russian], edited by S. S. Kutateladze, Izd. SO AN SSSR, 1964.