Comparison of Separation Control Mechanisms for Synthetic Jet and Plasma Actuators
This study numerically investigated the mechanisms of separation control using a synthetic jet (SJ) and plasma actuator (PA) around an NACA0015 airfoil at the chord Reynolds number of 63,000. Both SJ and PA were installed on the leading edge with the same order of input momentum (<inline-formula&...
Main Authors: | , , , , |
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Format: | Article |
Language: | English |
Published: |
MDPI AG
2023-08-01
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Series: | Actuators |
Subjects: | |
Online Access: | https://www.mdpi.com/2076-0825/12/8/322 |