Research Article
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 |
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