Research Article
On the Deflexion of Anisotropic Structural Composite Aerodynamic Components
Table 2
Predicted maxima strain values.
| | Model | Formulation | Maximum strain value (%) | Distance from root (m) | Proportion of length (%) |
| | Analytical (antiderivative) | Shell | 0.28 | 1.97 | 47 | | ANSYS (FE) | Shell | 0.29 | 2.05 | 48 | | Runge-Kutta (FD) | Solid | 0.28 | 1.84 | 44 | | Runge-Kutta (FD) | Shell | 0.28 | 1.84 | 44 |
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