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: | Комплексный метод оценки для выбора начальных параметров числа ступеней турбины и компрессора при проектировании проточной части турбовентиляторного двигателя |
| Authors: | Батурин О. В. Матвеев В. Н. |
| Keywords: | bypass ratio bypass turbojet engines engine mass engine thrust flow path design fuel consumption integrated evaluation method parameter selection pressure increase ratio stage number change turbofan engines выбор параметров двухконтурные турбореактивные двигатели изменение числа ступеней комплексный метод оценки масса двигателя проектирование проточной части расход топлива степень двухконтурности степень повыщения давления турбовентиляторные двигатели тяга двигателя |
| Issue Date: | 2025 |
| Citation: | Лю Синь Комплексный метод оценки для выбора начальных параметров числа ступеней турбины и компрессора при проектировании проточной части турбовентиляторного двигателя = Comprehensive assessment method for selecting initial parameters of the number of turbine and compressor stages when designing the flow passage of a turbofan engine / Лю Синь, О. В. Батурин, В. Н. Матвеев // 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. 863-865. |
| Abstract: | This paper comprehensively considers engine weight, thrust, bypass ratio, total pressure ratio and unit fuel consumption to give a selection scheme for the number of turbine stages. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/43391 |
| Appears in Collections: | Перспективы развития двигателестроения |
| File | Size | Format | |
|---|---|---|---|
| 978-5-7883-2191-2_2025-863-865.pdf | 461.52 kB | Adobe PDF | View/Open |
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