A Finite Element Formulation for Bending-Torsion Coupled Vibration Analysis of Delaminated Beams under Combined Axial Load and End Moment

<div>Changes of the nondimensional first and second natural frequencies (λ2) with respect to normalized buckling load P0/Pcr for H2/H = 0.3, Mzz/Mb = 0.4, and different values of L2/L.</div>

Shock and Vibration

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Figure 6

Figure 6: A Finite Element Formulation for Bending-Torsion Coupled Vibration Analysis of Delaminated Beams under Combined Axial Load and End Moment 