Abstract
A method is described for integrating on a MN-7 analog computer the energy equations relevant to a moving medium with heat sources, for the two-dimensional adiabatic problem, allowing for compressibility. Jet temperature and velocity fields for accompanying flows in the combustion of methane, obtained by machine integration, are presented.
This is a preview of subscription content, log in via an institution to check access.
Similar content being viewed by others
References
A. P. Kovalev, A. S. Ippolitov, and Chuang Feng-ch'eng, IFZh, no. 5, 1963.
A. P. Kovalev, A. S. Ippolitov, Yu. M. Torgonenko, Debdas Bkhaduri, Yu. R. Schneider, and N. I. Chelnokov, IFZh, no. 10, 1964.
A. G. Prudnikov, Third All-Union Congress on Combustion Theory, 1 [in Russian], Izd. In-ta Khimicheskoi fiziki AN SSSR, 1960.
L. A. Vulis, Investigation of the Physical Basis of Operation of Furnaces and Ovens [in Russian], Izd. AN Zaz. SSR, 1957.
B. P. Demidovich, I. A. Maron, and E. Z. Shuvalova, Numerical Methods of Analysis [in Russian], FM, 1963.
G. N. Abramovich, Theory of Turbulent Jets [in Russian], GEI, 1960.
G. K. Sobolev, IFZh, no. 3, 1960.
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Dvoinishnikov, V.A., Ippolitov, A.S. Jet configuration in accompanying flows. Journal of Engineering Physics 11, 140–145 (1966). https://doi.org/10.1007/BF00831272
Issue Date:
DOI: https://doi.org/10.1007/BF00831272