Numerical Analysis of Free Play-Induced Aeroelastic Phenomena: A Numerical Approach With Adaptive Step Size Control

Table 1

Structural parameters of the aeroelastic model.

Parameter	Value
Semichord length ()	0.127 m
Span length	0.52 m
Elastic axis ()	−0.5 b
Mass of wing ()	3.293 kg
Static mass moment ()	0.08587 kg∙m
Location of C.G. ()	0.434
Translational stiffness ()	2818.8 N/m
Rotational stiffness ()	37.3 N∙m/rad
Structural damping ()	2.105 Nm∙s/m
Structural damping ()	0.0225 Nm∙s/rad