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This article is cited in 4 scientific papers (total in 4 papers)
Electrification of nozzle in a liquid rocket engine
D. A. Yagodnikov, A. V. Voronetskii, N. M. Pushkin Institute of Power Engineering, Moscow 107005
Abstract:
A method of electrical-physical diagnostics is developed and experimental studies are conducted of the process of nozzle electrification in a liquid rocket engine operating on a hydrocarbon fuel. The highest electric potential is shown to be realized at about a stoichiometric ratio of the components, i.e., when the flow velocity, temperature, and, hence, ionization of combustion products are maximum. Recommendations for practical application of the information obtained are given.
Received: 26.01.1994
Citation:
D. A. Yagodnikov, A. V. Voronetskii, N. M. Pushkin, “Electrification of nozzle in a liquid rocket engine”, Fizika Goreniya i Vzryva, 31:4 (1995), 54–58; Combustion, Explosion and Shock Waves, 31:4 (1995), 450–454
Linking options:
https://www.mathnet.ru/eng/fgv2806 https://www.mathnet.ru/eng/fgv/v31/i4/p54
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