Abstract
An experimental study was made of the heat transfer distribution during gas injection into the supersonic region of a Laval nozzle. The dimensionless parameters governing this process have been established as a result.
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N. M. Tsirel'man, F. G. Bakirov, and Z. G. Shaikhutdinov, Inzh. Fiz. Zh.,24, No. 2 (1973).
A. V. Lykov, Theory of Heat Conduction [in Russian], Izd. Vysshaya Shkola, Moscow (1967).
A. L Glagolev et al., Izv. Akad. Nauk SSSR, Mekhan. Zhidk. i Gaza, No. 3 (1967).
D. M. Voitenko et al., Izv. Akad. Nauk SSSR,Mekhan. Zhidk. i Gaza, No. 1 (1966).
D. A. Needham, Rocket Engrg. and Cosmonautics [Russian translation],3, No. 4 (1965).
A. A. Gukhman, Introduction to the Theory of Similarity [in Russian], Izd. Vysshaya Shkola, Moscow (1967).
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 24, No. 5, pp. 790–797, May, 1973.
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Bakirov, F.G., Shaikhutdinov, Z.G. Characteristics of heat transfer in the region of gas injection into a supersonic high-temperature gas stream. Journal of Engineering Physics 24, 558–563 (1973). https://doi.org/10.1007/BF00838611
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DOI: https://doi.org/10.1007/BF00838611