A Semianalytical Three-Dimensional Elasticity Solution for Vibrations of Orthotropic Plates with Arbitrary Boundary Conditions

<div>Variation of the first ten frequencies (Hz) against material parameter <i>η</i> (<i>η</i> = E11/E22) for a thick plate with different boundary conditions: (a) CCCC; (b) SSSS; (c) E1E1E1E1; (d) E4E4E4E4.</div>

Shock and Vibration

fig12

Figure 12

Figure 12: A Semianalytical Three-Dimensional Elasticity Solution for Vibrations of Orthotropic Plates with Arbitrary Boundary Conditions 