Control of nozzle flow using microjets at supersonic Mach Regime

• 主要な著者: G M, Fharukh, Khan, Sher Afghan
• フォーマット: 論文
• 言語: English; English; English
• 出版事項: Materials and Energy Research Center 2019
• 主題: TL Motor vehicles. Aeronautics. Astronautics; TL780 Rockets
• オンライン･アクセス: http://irep.iium.edu.my/73710/1/73710_Control%20of%20Nozzle%20Flow%20Using%20Microjets.pdf; http://irep.iium.edu.my/73710/2/73710_Control%20of%20Nozzle%20Flow%20Using%20Microjets_SCOPUS.pdf; http://irep.iium.edu.my/73710/13/73710_Control%20of%20Nozzle%20Flow%20Using%20Microjets_wos.pdf; http://irep.iium.edu.my/73710/; http://www.ijeir.info/article_91333_2d09bd719a0f0622b9f62887c333b092.pdf

This article reports the active control of base flows using the experimental procedure. Active control of base pressure helps in reducing the base drag in aerodynamic devices having suddenly expanded flows. Active control in the form of microjets having 0.5 mm radius placed at forty-five degrees apa...