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