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Разработка программного комплекса для расчета течений продуктов сгорания в проточном тракте РДТТ с учетом изменения геометрии наполнителя К. В. Костюшин, М. С. Середа, А. В. Червакова

By: Костюшин, Кирилл ВладимировичContributor(s): Середа, Михаил Сергеевич | Червакова, Анастасия ВладимировнаMaterial type: ArticleArticleContent type: Текст Media type: электронный Other title: Development of program for calculation of gas flows in a solid-fuel rocket engine with a moving geometry [Parallel title]Subject(s): разработка программных комплексов | ракетные двигатели на твердом топливе | течение продуктов сгорания | газодинамические трактыGenre/Form: статьи в сборниках Online resources: Click here to access online In: Перспективы развития фундаментальных наук. Т. 3 : сборник научных трудов XVI Международной конференции студентов, аспирантов и молодых ученых, 23-26 апреля 2019 г Т. 3 : Математика. С. 71-73Abstract: In the present study calculations algorithm of gas flow in solid-fuel rocket engine are shown. The algorithm is based on the solution of two-dimensional gas dynamics equations. Calculations are done for solidfuel rocket engine model which consists of combustion chamber and nozzle. The results in agreement with known solutions.
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In the present study calculations algorithm of gas flow in solid-fuel rocket engine are shown. The
algorithm is based on the solution of two-dimensional gas dynamics equations. Calculations are done for solidfuel
rocket engine model which consists of combustion chamber and nozzle. The results in agreement with known
solutions.

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