Experimental study on flow around airfoil by using dielectric barrier discharge (DBD) plasma actuator
This experimental study was focused on the usage of DBD plasma actuator for enhancement aerodynamic performance of airfoil model NACA 0015. The DBD plasma actuator was able to suppress flow separation near the leading edge by disturbing airflow near that region. It can be seen that continuous small...
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Asian Research Publishing Network,
2018-04.
|
| Subjects: | |
| Online Access: | Get fulltext |