Effect of the gasdynamics of a two-regime combustor on the power characteristics of a model with combustion

Author:

Baev V. K.,Shumskii V. V.

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Reference19 articles.

1. V. K. Baev, V. V. Shumskii, and M. I. Yaroslavtsev, “Some methodology aspects in the investigation of gasdynamic models with heat mass supply in an aerodynamic shock tube,” Fiz. Goreniya Vzryva,23, No. 5, 45–54 (1987).

2. V. K. Baev, V. V. Shumskii, and M. I. Yaroslavtsev, “Study of combustion and heat exchange processes in high-enthalpy short-duration facilities,” High-Speed Flight Propulsion Systems. Progress in Astronautics and Aeronautics,137 (1991).

3. V. K. Baev, V. V. Shumskii, and M. I. Yaroslavtsev, “Investigation of the power characteristics and the flow parameters in the channel of a model with combustion,” Prikl. Mekh. Tekh. Fiz., No. 1 (1984).

4. Yu. A. Saren and V. V. Shumskii, “Characteristics of a hypersonic ramjet engine with a two-regime combustion chamber,” in: Gasdynamics of the Flow through Nozzles and Diffusers [in Russian], Novosibirsk (1982).

5. E. A. Meshcheryakov and V. A. Sabel'nikov, “Hydrogen combustion in a supersonic turbulent flow through a channel with accompanying fuel and oxidizer feed,” Fiz. Goren. Vzryva,12, No. 2, 55–64 (1981).

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