Abstract
A new numerical algorithm for simulation of nonequilibrium chemically reacting flows of an inviscid multicomponent gas is described. Application of this algorithm to the numerical solution of several problems of air-hydrogen mixture combustion in oblique detonation waves is demonstrated.
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Additional information
Zhukovskii Central Aerodynamic Institute, Zhukovskii 140160. Translated from Fizika Goreniya i Vzryva, Vol. 31, No. 3, pp. 118–133, May–June, 1995.
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Vlasenko, V.V., Sabel'nikov, V.A. Numerical simulation of inviscid flows with hydrogen combustion behind shock waves and in detonation waves. Combust Explos Shock Waves 31, 376–389 (1995). https://doi.org/10.1007/BF00742685
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DOI: https://doi.org/10.1007/BF00742685