DRAG INVESTIGATION AROUND A CYLINDER AND SYMMETRIC AIRFOIL IN TANDEM WITH DIFFERENT GAPS AND ANGLES OF ATTACK
A Numerical simulation for the turbulent airflow around a symmetrical airfoil (NACA 0012) adjusted in tandem with circular cylinder, the airfoil were adjusted at variable angle of attack between (5-20°) with positive clockwise inclination setting the cylinder center in front of the leading-edge ce...
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Zibeline International
2019-01-01
|
| Series: | Journal of Mechanical Engineering Research and Developments |
| Subjects: | |
| Online Access: | https://jmerd.org.my/Paper/Vol.42,No.1(2019)/26-33.pdf |