| Title: | Методика оптимизации входного устройства силовой установки летательного аппарата типа «летающее крыло» |
| Other Titles: | Design optimization of the power plant inlet for blended wing-body aircraft |
| Authors: | Агульник, А.Б. Юрлова, Н.Ю. |
| Issue Date: | 2016 |
| Publisher: | Самарский университет |
| Citation: | Материалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 1, с. 186 |
| Abstract: | The paper deals with design optimization of inlet designed to blended wing-body for the performance improvement. As a result, the configuration of the inlet has been found to improve performances for two regimes: taking off and cruising flight. |
| Description: | УДК 621. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/15313 |
| ISBN: | 978-5-7883-1084-8 |
| Appears in Collections: | Проблемы и перспективы развития двигателестроения |
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