Base Pressure Control using Micro-jets in Supersonic Flow Regimes
نویسندگان
چکیده
منابع مشابه
Control of Nozzle Flow Using Microjets at Supersonic Mach Regime
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 apart is employed to control the base pressure. The Mach numbers of the present analysis are 1.7, 2....
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ژورنال
عنوان ژورنال: International Journal of Aviation, Aeronautics, and Aerospace
سال: 2018
ISSN: 2374-6793
DOI: 10.15394/ijaaa.2018.1148