| 摘要 |
The invention relates to a method for calculating a trailing edge to be produced for a rotor blade of an aerodynamic rotor of a wind turbine, wherein the rotor blade has radial positions in relation to the rotor, the rotor blade has a local blade profile that depends on radial positions related to the rotor, and the trailing edge has a toothed course having several teeth, wherein each tooth has a tooth height and a tooth width, and the tooth height and/or the tooth width is calculated in dependence on the radial position of the tooth and/or in dependence on the local blade profile of the radial position of the tooth. |
