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