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Расчет потерь на химическую неравновесность в соплах ракетных двигателей А. В. Червакова, К. В. Костюшин
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ArticleContent type: Текст Media type: электронный Other title: Calculation of losses for chemical inequality in rocket engine nozzles [Parallel title]Subject(s): сопла ракетных двигателей | математическое моделирование | продукты сгорания | химическая неравновесностьGenre/Form: статьи в сборниках Online resources: Click here to access online
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Перспективы развития фундаментальных наук. Т. 3 : сборник научных трудов XVIII Международной конференции студентов, аспирантов и молодых ученых, 27–30 апреля 2021 г Т. 3 : Математика. С. 91-93Abstract: An algorithm has been developed that makes it possible to calculate the reacting flows of combustion products in the nozzles of rocket engines. Calculations of the flow of combustion products of model fuel for a test configuration of a rocket engine with a radius-conical nozzle are carried out. Specific impulse losses due to chemical nonequilibrium in the gas phase are determined.
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An algorithm has been developed that makes it possible to calculate the reacting flows of combustion products in the nozzles of rocket engines. Calculations of the flow of combustion products of model fuel for a test configuration of a rocket engine with a radius-conical nozzle are carried out. Specific impulse losses due to chemical nonequilibrium in the gas phase are determined.
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