Research Article
On the Deflexion of Anisotropic Structural Composite Aerodynamic Components
Table 1
Tapered elliptical beam models maximum deflexion predictions.
| | Model | Formulation | Maximum displacement |
| | Runge-Kutta (FD) | Solid | 363.4 mm | | Anti-derivative | Shell | 363.7 mm | | Runge-Kutta (FD) | Shell | 363.7 mm | | Finite element (FE) | ANSYS-shell | 358.2 mm | | Finite element (FE) | CATIA-shell | 357.0 mm |
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