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: | Инструмент анализа результатов экспериментального определения параметров неоднородного потока на входе в компрессор авиационного ГТД |
| Authors: | Пестов Д. В. |
| Keywords: | aircraft gas turbine engines compressors degree of flow non-uniformity experimental results gas-dynamic stability measurement errors method for determining confidence limits non-uniform flow parameters авиационные газотурбинные двигатели газодинамическая устойчивость компрессоры метод определения доверительных границ параметры неоднородного потока погрешности измерений результаты эксперимента степень неоднородности потока |
| Issue Date: | 2025 |
| Citation: | Пестов, Д. В. Инструмент анализа результатов экспериментального определения параметров неоднородного потока на входе в компрессор авиационного ГТД = A tool for analyzing the results of experimental determination of inhomogeneous flow parameters at the entrance to the compressor of the aviation gas turbine engine / Д. В. Пестов // 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. 957-959. |
| Abstract: | In the production of serial aviation gas turbine engines (GTD) and engines after repair, special tests are carried out to confirm gas dynamic stability as part of the acceptance testing program. Since the late 70s, on the recommendation of the CIAM, such tests have been performed with a simulation of an inhomogeneous flow at the inlet to gas turbine engine. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/43240 |
| Appears in Collections: | Перспективы развития двигателестроения |
| File | Size | Format | |
|---|---|---|---|
| 978-5-7883-2191-2_2025-957-959.pdf | 281.03 kB | Adobe PDF | View/Open |
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