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From discussion here; Groups link, twist is set in the horizontal plane, not relative to the actual angle of the wing. This means that winglets cannot be modelled with twist or toe angles, other than by modifying the section theta.
This is therefore a feature request to add an option to either make the twist angle relative to the dihedral of the wing or to add another parameter to set the section angle in the horizontal as well as the vertical plane.
The text was updated successfully, but these errors were encountered:
From discussion here; Groups link, twist is set in the horizontal plane, not relative to the actual angle of the wing. This means that winglets cannot be modelled with twist or toe angles, other than by modifying the section theta.
This is therefore a feature request to add an option to either make the twist angle relative to the dihedral of the wing or to add another parameter to set the section angle in the horizontal as well as the vertical plane.
The text was updated successfully, but these errors were encountered: