Numerical modeling of the flow of combustion products of a fuel containing a boron–aluminum admixture in the nozzle of a solid-propellant rocket engine has been carried out. The advantage of boron–aluminum over aluminum in using in composite solid propellants has been shown.
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 93, No. 6, pp. 1397–1402, November–December, 2020.
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D’yachenko, N.N., D’yachenko, E.N. Digital Simulation of a High-Energy System Using a Boron–Aluminum Admixture as a Fuel. J Eng Phys Thermophy 93, 1347–1352 (2020). https://doi.org/10.1007/s10891-020-02240-2
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DOI: https://doi.org/10.1007/s10891-020-02240-2