2017.23
Session ID : 203
Conference information
Host: The Japan Society of Mechanical Engineers
Name : [in Japanese]
Date : March 16, 2017 - March 17, 2017
Trailing edge flow separation control using Feedback driven Plasma Actuator triggered by fluctuating velocity in the wake of an NACA0012 Airfoil.
Keywords:
Plasma Actuator,
NACA0012 Airfoil,
Feedback,
Trailing edge flow separation control,
Low Reynolds Number
Details
Article 1st page
