Technology of computational analysis of the working process parameters of low-thrust rocket engines running on gaseous oxygen-hydrogen fuel with the use of ANSYS CFD

Συγγραφείς: V. V. Ryzhkov, I. I. Morozov

Πηγή: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 18, Iss 2, Pp 62-74 (2019)

Θεματικοί όροι: model of the working process, 0103 physical sciences, technology of computational analysis, distribution of parameters in the gas-dynamic path, TL1-4050, gaseous oxygen-hydrogen fuel, Low-thrust rocket engine, 7. Clean energy, 01 natural sciences, parametric study, Motor vehicles. Aeronautics. Astronautics, 0105 earth and related environmental sciences

Σύνδεσμος πρόσβασης: https://journals.ssau.ru/index.php/vestnik/article/download/6742/6611
https://doaj.org/article/b1f46900ffde457ab0e77065dd3c3161
https://journals.ssau.ru/index.php/vestnik/article/view/6742
https://journals.ssau.ru/vestnik/article/download/6742/6611