Samara University Repository
Welcome to the Samara University repository!
This is an open electronic archive created to preserve and disseminate the scientific results of our university. The works of researchers, faculty members, and students are available to everyone for academic and research purposes.
The repository contains dissertations, research articles, educational and methodological materials, monographs, and regulatory documents. The collections cover a wide range of fields: from aerospace technologies, engine engineering, and computer science to history, linguistics, mathematics, and ecology. The archive brings together the scientific heritage of the university, including materials prepared during the period of Samara State Aerospace University and Samara State University.
Looking for publications by author, title, date, or subject? Full-text search will provide relevant results. Want to explore the academic life more closely? Browse materials by the universityâs organizational units.
Descriptions of all publications and articles available in the repository can be found in the libraryâs electronic catalog. Staff and students can log in via the menu "Login -> My Resource Archive" using their personal account credentials (SSAU_id).
Use the archive for study, research, and professional development!
| Title: | Расчет нестационарного теплового состояния соплового блока ракетного двигателя на твердом топливе |
| Authors: | Уланов Д. Д. Ворожеева О. А. |
| Keywords: | математическое моделирование тепловое состояние температурные поля сопловый блок ракетные двигатели твердого топлива thermal state temperature fields solid-fuel rocket engines nozzle block mathematical modeling |
| Issue Date: | 2025 |
| Citation: | Уланов, Д. Д. Расчет нестационарного теплового состояния соплового блока ракетного двигателя на твердом топливе = Calculation of the transient thermal state of the nozzle block of a solid fuel rocket engine / Д. Д. Уланов, О. А. Ворожеева // Перспективы развития двигателестроения : материалы междунар. науч.-техн. конф. им. Н. Д. Кузнецова (18–20 июня 2025 г.) / Самар. нац. исслед. ун-т им. С. П. Королева (Самар. ун-т) ; редкол.: Е. В. Шахматов, А. И. Ермаков. - Самара : Изд-во Самар. ун-та, 2025. - С. 984-985. |
| Abstract: | The work presents a numerical simulation of the non-stationary thermal state of the nozzle block of a solid-fuel rocket engine operating in outer space. The mathematical model takes into account the features of heat exchange on the inner and outer walls of the nozzle block, as well as the properties of the structural materials. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/43495 |
| Appears in Collections: | Перспективы развития двигателестроения |
| File | Size | Format | |
|---|---|---|---|
| 978-5-7883-2191-2_2025-984-985.pdf | 252.97 kB | Adobe PDF | View/Open |
Items in Repository are protected by copyright, with all rights reserved, unless otherwise indicated.