TY  - GEN
AU  - Середа,Михаил Сергеевич
AU  - Костюшин,Кирилл Владимирович
TI  - Программный комплекс расчета течения продуктов сгорания в проточных трактах с учетом нестационарного газоприхода и нагрева конструкции ракетного двигателя
KW  - программные комплексы
KW  - ракетные двигатели
KW  - продукты сгорания
KW  - вычислительные эксперименты
KW  - статьи в сборниках
N1  - Библиогр.: 5 назв
N2  - The article presents a program designed for mathematical modeling of non-stationary processes in the flow part of a solid-fuel rocket engine and heating of the engine structure by combustion products. The solution of this problem is an important stage in the design of rocket engines. Of great interest to this work is its main goal: the development of a universal domestic application that allows you to simulate gas-dynamic and thermophysical processes with high-quality output results. The development of the software package was carried out in the C# language in the environment Microsoft Visual Studio 2019. The construction of a rich graphical interface of the software package is implemented using WPF (Windows Presentation Foundation) technology, using the declarative markup language XAML. Mathematical modeling of non-stationary gas-dynamic processes in the flow paths of a rocket engine is carried out by methods based on the solution of the complete Euler equations. Modeling of the heating process of the rocket engine structure is described by the equation of thermal conductivity
UR  - http://vital.lib.tsu.ru/vital/access/manager/Repository/koha:000846785
ER  -