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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2001, Volume 42, Issue 1, Pages 25–32
(Mi pmtf2708)
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This article is cited in 2 scientific papers (total in 2 papers)
Gas–dynamic structures in supersonic combustion of hydrogen in a system of plane jets in a supersonic flow
U. Ê. Zhapbasbaev, Y. P. Makashev Al–Farabi Kazakh National State University, Almaty, 480121
Abstract:
Results of numerical and theoretical studies of supersonic diffusive combustion of a system of plane hydrogen jets in a supersonic air flow are described. It is shown that large–scale vortex structures appear in the mixing zone of the system of hydrogen jets and the cocurrent flow. These vortex structures affect the mechanism of turbulent exchange between the fuel and the oxidizer.
Received: 22.07.1999 Accepted: 11.01.2000
Citation:
U. Ê. Zhapbasbaev, Y. P. Makashev, “Gas–dynamic structures in supersonic combustion of hydrogen in a system of plane jets in a supersonic flow”, Prikl. Mekh. Tekh. Fiz., 42:1 (2001), 25–32; J. Appl. Mech. Tech. Phys., 42:1 (2001), 21–27
Linking options:
https://www.mathnet.ru/eng/pmtf2708 https://www.mathnet.ru/eng/pmtf/v42/i1/p25
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