| Title: | Сравнительное исследование эффективности плёночного охлаждения сопловых лопаток турбины с цилиндрическими и профилированными отверстиями в адиабатных и сопряжённых условиях |
| Other Titles: | 3D investigation of film cooling effectiveness for turbine nozzle vane with cylindrical, fan shaped and laidback fan-shaped film-cooling holes in adiabatic and conjugate conditions |
| Authors: | Горелов, Ю.Г. Тюльков, К.В. |
| Issue Date: | 2016 |
| Publisher: | Самарский университет |
| Citation: | Материалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 1, с. 9-11 |
| Abstract: | In order to optimize the vane film cooling and thereby increase the efficiency of a gas turbine, different film cooling configurations were computationally investigated. A computational study is carried out for comparison of the effectiveness of film cooling through holes of different shapes: cylindrical, fan-shaped, and laidback fan-shaped film-cooling holes in adiabatic and conjugate conditions. |
| Description: | УДК 621.438-226.2.048 |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/14488 |
| ISBN: | 978-5-7883-1084-8 |
| Appears in Collections: | Проблемы и перспективы развития двигателестроения |
Items in Repository are protected by copyright, with all rights reserved, unless otherwise indicated.