respect to the original one, increasing the correlation between the multibody model and the experimental modal results. Figure 6 shows a comparison between some of the experimental and numerical mode shapes. a) Tower fore-aft bending experimental b) Tower fore-aft bending numerical c) 1st rotor flap asymmetric experimental d) 1st rotor flap asymmetric numerical e) 1st rotor flap symmetric experimental f) 1st rotor flap symmetric numerical Fig. 6 Comparison between some of the experimental and numerical mode shapes 356
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