Research Article
Effect of Aeroelastic Tailoring Design on Wing Mode
Table 4
Carbon fibre composite epoxy carbon UD (230 GPa) material parameters [
35].
| | Density (kg/m3) | Modulus of elasticity (GPa) | Shear elasticity (GPa) | Poisson’s ratio | | | | | | | | | |
| | 1490 | 121 | 8.6 | 8.6 | 4.7 | 3.1 | 4.7 | 0.27 | 0.4 | 0.27 |
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