Abstract
The problem of determining the “potential” number of integration steps by explicit difference schemes is solved within the framework of the prediction model for chemically non-equilibrium processes.
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Original Russian Text © V.G. Kryukov, A.L. Abdullin, A.V. Demin, 2017, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2017, No. 1, pp. 98–103.
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Kryukov, V.G., Abdullin, A.L. & Demin, A.V. Difference schemes in computations for chemically non-equilibrium processes in the rocket engine nozzles. Russ. Aeronaut. 60, 103–109 (2017). https://doi.org/10.3103/S1068799817010159
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DOI: https://doi.org/10.3103/S1068799817010159