Problem description
Model:
Isotropic mass | |
100.0 | |
Anisotropic mass | |
100.0 | |
200.0 | |
300.0 | |
Rotary inertia | |
100.0 | |
200.0 | |
300.0 | |
Centrifugal axis of rotation | (0, 0, 1) through (0, 0, 0) |
Gravity load vector | (0, 1, 0) |
Rotary acceleration axis | (0, 0, 1) through (0, 0, 0) |
General:
The ROTARYI element and anisotropic MASS element are also tested with local coordinate systems and with finite rotation.