Research Article
Flight Loads Prediction of High Aspect Ratio Wing Aircraft Using Multibody Dynamics
Table 5
Trim angle of attack and CPU time: linear FEM versus multibody results.
| Load factor [g] | Linear trim FEM | Trim multibody | α [deg] | CPU time [s] | α [deg] | CPU time [s] |
| 1 | 4.91 | <1 | 5.04 | 103.0 | 2.5 | 12.28 | <1 | 13.40 | 70.3 |
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