Samara University Repository
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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.
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| Title: | Расчет нестационарного температурного состояния деталей двигателя по граничным условиям III рода, полученным из двумерного теплогидравлического расчета |
| Authors: | Дегтярев Н. Д. Мордвинцев М. Ю. Мусеев А. А. |
| Keywords: | boundary conditions of the third kind gas turbine engine parts hydraulic modeling non-stationary temperature fields secondary air system temperature states thermo-hydraulic models вторичная воздушная система гидравлическое моделирование граничные условия третьего рода детали газотурбинных двигателей нестационарные температурные поля температурные состояния термогидравлические модели |
| Issue Date: | 2025 |
| Citation: | Дегтярев, Н. Д. Расчет нестационарного температурного состояния деталей двигателя по граничным условиям III рода, полученным из двумерного теплогидравлического расчета = Calculation of an unsteady-state temperature field for a gas-turbine parts using third kind boundary conditions obtained from a two-dimensional thermohydraulic model / Н. Д. Дегтярев, М. Ю. Мордвинцев, А. А. Мусеев // 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. 29-31. |
| Abstract: | There is a calculation method, which is allowing to obtain an nsteady-state temperature field for a gas-turbine engine’s parts using third kind boundary conditions obtained from a two-dimensional thermohydraulic model. The main benefit of this method is probability to save time because the direct 3D calculations of conjugate heat transfer no more needed. In current article details of algorithm, method and its validation are represented. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/43191 |
| Appears in Collections: | Перспективы развития двигателестроения |
| File | Size | Format | |
|---|---|---|---|
| 978-5-7883-2191-2_2025-29-31.pdf | 258.9 kB | Adobe PDF | View/Open |
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