Corotational Finite Element Dynamic Analysis of Space Frames with Geometrically Nonlinear Behavior Based on Tait–Bryan Angles

<div>Time-displacement <i>U</i><sub><i>X</i></sub> of the point <i>A</i> curve for the cantilever beam.</div>

Shock and Vibration

Figure 26: Corotational Finite Element Dynamic Analysis of Space Frames with Geometrically Nonlinear Behavior Based on Tait–Bryan Angles 