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J. A. D. Ackroyd, “A study on the running times in reflected shock tunnels,” Aeronaut. Res. Council, Current Papers, No. 883 (1967).
H. O. Amann, “Vorgange beim Start einer ebenen Reflexionsduse,” Z. Flugwiss.,19, No. 10 (1971).
H. O. Amann, “Experimental study of the starting process in a reflection nozzle,” Phys. Fluids,12, No. 5 (1969).
C. E. Smith, “An analytic study of a starting process in a hypersonic nozzle,” in: 1964 Proceedings of the Heat Transfer and Fluid Mechanics Institute, Standford University Press, Stanford (1964).
C. E. Smith, “The starting process in a hypersonic nozzle,” J. Fluid Mech.,24, No. 4 (1966).
R. Marmey and J. P. Guibergia, “Etude experimentale des phenomenes accompagnant l'amorgage d'une tuyere hypersonic,” Compt. Rend. Acad. Sci., Ser. A,271, No. 2
D. Migdal and F. Landis, “Characteristics of conical supersonic nozzles” ARS J.,32, No. 12 (1962).
L. Beck and R. Kaffel, “Determination of oblique compression shocks ina conical nozzle with critical section in the form of two circles,” Raketn. Tekh. Kosmonavt.,4, No. 12 (1966).
P. K. Chang, Separation of Flow, Pergamon (1969).
G. Yu. Stepanov and L. V. Gogish, Quasi-one-dimensional Gasdynamics of Rocket Motor Nozzles [in Russian], Mashinostroenie, Moscow (1973).
A. Mager, “On the model of the free, shock-separated, turbulent boundary layer,” J. Aeronaut. Sci.,23, No. 2 (1956).
M. Summerfield, C. R. Foster, and W. C. Swan, “Flow separation in overexpanded supersonic nozzles,” Jet Propuls.,24, No. 5 (1954).
G. E. Gadd, “Interactions between wholly laminar or wholly turbulent boundary layers and shock waves strong enough to causes separation,” J. Aeronaut. Sci.,20, No. 11 (1953).
Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 1, pp. 76–82, January–February, 1977.
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Gvozdeva, L.G., Zhilin, Y.V. Formation of a quasistationary jet within a nozzle during its shock start-up. Fluid Dyn 12, 63–67 (1977). https://doi.org/10.1007/BF01074626