Estimating the applicability of kinetic schemes in hydrogen combustion simulation in combustion chambers of aircraft engines
2021 ◽
Vol 2057
(1)
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pp. 012068
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Abstract This paper presents the results of numerical simulation of hydrogen combustion in a supersonic flow of an oxidizing medium in a model combustion chamber using various models of chemical kinetics. The best scheme, which most accurately describes the combustion processes, is revealed. Comparison of the calculated distribution of molar fractions with experimental data is carried out, and relative deviations for the piloted mode of operation of the chamber are obtained.
2008 ◽
Vol 602
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pp. 209-218
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1981 ◽
Vol 103
(1)
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pp. 34-42
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2000 ◽
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1984 ◽
Vol 49
(1)
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pp. 170-178
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2014 ◽
Vol 529
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pp. 102-107
1996 ◽
Vol 118
(2)
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pp. 201-209
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