Research Article
Established Numerical Techniques for the Structural Analysis of a Regional Aircraft Landing Gear
Table 4
Static and dynamic loading conditions (stick model).
| | | Rx (N) | Ry (N) | Rz (N) |
| | Node 52 | | | | | Stick static load | 25293 | 3453 | −160003 | | Stick dynamic load | −14420 | −97770 | −35078 |
| | Node 55 | | | | | Stick static load | 17395 | −261989 | 54479 | | Stick dynamic load | 102047 | −154301 | −350578 |
| | Node 66 | | | | | Stick static load | −42688 | 258536 | −52077 | | Stick dynamic load | −87626 | 252071 | −177144 |
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