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Разработка программы расчета газодинамических характеристик течения и потерь тяги на трение в сопловом блоке с центральным телом В. Н. Конев, К. В. Костюшин
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ArticleContent type: Текст Media type: электронный Other title: Development of a program for calculation of gas-dynamic characteristics of the flow and loss of throat for friction in a nozzle unit with a central body [Parallel title]Subject(s): твердотопливные ракетные двигатели | сопла ракетных двигателей | газодинамические характеристики | математическое моделированиеGenre/Form: статьи в сборниках Online resources: Click here to access online
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Перспективы развития фундаментальных наук. Т. 3 : сборник научных трудов XIX Международной конференции студентов, аспирантов и молодых ученых, 26-29 апреля 2022 г Т. 3 : Математика. С. 27-29Abstract: A method and algorithm for calculating the gas dynamic characteristics of the flow and thrust losses due to friction and scattering in the nozzle block of a rocket engine have been developed. Based on the developed algorithm, a specialized software package is implemented to calculate the flow and thrust losses in a nozzle with or without a central body.
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A method and algorithm for calculating the gas dynamic characteristics of the flow and thrust losses due to friction and scattering in the nozzle block of a rocket engine have been developed. Based on the developed algorithm, a specialized software package is implemented to calculate the flow and thrust losses in a nozzle with or without a central body.
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