Development of mathematical model of processes in gas generator with unitary fuel for powering turbine of liquid rocket engine
| Autor: | A. B. Yakovlev |
|---|---|
| Jazyk: | English<br />Russian |
| Rok vydání: | 2023 |
| Předmět: | |
| Zdroj: | Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", Vol 7, Iss 3, Pp 82-88 (2023) |
| Druh dokumentu: | article |
| ISSN: | 2588-0373 2587-764X |
| DOI: | 10.25206/2588-0373-2023-7-3-82-88 |
| Popis: | The article considers the dynamic model of a gas generator with control throttle of liquid rocket engine with pumping supply system and unitary fuel for powering the turbine. The system of dynamic equations describing the processes occurring in a single-component gas generator and a throttle valve is obtained. The mathematical model makes it possible to analyze and identify the main patterns of the influence of input quantities on the controlled quantity. |
| Databáze: | Directory of Open Access Journals |
| Externí odkaz: |
|