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 |