Research Article

Aeroelastic Optimization Design for High-Aspect-Ratio Wings with Large Deformation

Table 7

Comparison of modal results after linear optimization and nonlinear analysis.

Mode DescriptionFrequency (Hz)Diff. (%)
Linear optimizationNonlinear reanalysis

1st vertical bending1.971.57−25.6%
1st chordwise bending2.752.16−27.4%
2nd vertical bending7.206.75−6.6%
2nd chordwise bending11.0210.45−5.4%
3rd vertical bending17.4716.97−3.0%
1st torsion27.0026.95−0.2%