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| Title: | Численное моделирование влияния геометрических параметров сопла на коэффициент расхода ДЛА |
| Other Titles: | The numerical simulation of the influence of nozzle's geometrical parameters on aircraft engines' discharge coefficient |
| Authors: | Сабирзянов, А.Н. Кириллова, А.Н. |
| Issue Date: | 2016 |
| Publisher: | Самарский университет |
| Citation: | Материалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 2, с. 39-40 |
| Abstract: | Multiparameter research of dependence of aircraft engine nozzle discharge coefficient on its geometrical parameters has been conducted using advanced CFD methods. Characteristic influence of a contour of supersonic section of the nozzle and its cylindrical section of the throat on nozzle discharge coefficient has been shown. |
| Description: | УДК 621.45.02+536.8+519.6 |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/14577 |
| ISBN: | 978-5-7883-1084-8 |
| Appears in Collections: | Проблемы и перспективы развития двигателестроения |
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