Table 1: Properties employed in the aerofoil model for the flow-induced vibration of the NACA 0015 aerofoil.
Parameters |
Values |
Units |
Chord |
59.5 |
mm |
Mass |
0.148 |
kg |
Linear Stiffness |
16.383 |
N/m |
Linear Damping |
5.6 |
kg/s |
Torsion Stiffness |
0.00753 |
N m/deg |
Torsion Damping |
0.00078 |
kg m2/s |