Leading-edge flow separation control over a NACA 0012 aerofoil with DBD plasma actuators

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Leading-edge flow separation control over a NACA 0012 aerofoil with DBD plasma actuators

An experimental investigation has been conducted in a low-speed wind tunnel at the University of Nottingham to study the flow separation control capability of a wall-normal plasma jet by DBD plasma actuator over a NACA 0012 aerofoil. As an active flow separation control technique, DBD plasma actuato...

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Bibliographic Details
Main Author:	Song, Longfei
Format:	Thesis (University of Nottingham only)
Language:	English
Published:	2018
Subjects:	flow control; DBD plasma actuator; separation; NACA 0012 aerofoil
Online Access:	https://eprints.nottingham.ac.uk/49841/

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