Active Stall Control System on NACA0012 by Using Synthetic Jet Actuator
نویسندگان
چکیده
منابع مشابه
experimental investigation of active flow control for changing stall angle of a naca0012 airfoil, using plasma-actuator
active flow control has great importance in design of flying objects in general and control flaps in particular. using dielectric barrier discharge as plasma actuators over control flaps can cause a change in position of separation point or can eliminate it. this new flow control device produces a body force that causes generating a micro wall jet. the present study aims to investigate experime...
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ژورنال
عنوان ژورنال: Journal of Flow Control, Measurement & Visualization
سال: 2019
ISSN: 2329-3322,2329-3330
DOI: 10.4236/jfcmv.2019.71005