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发明公开
CN104704233A 燕尾型翼 有权 转让

燕尾型翼
摘要：
一种空气动力元件，该空气动力元件的横截面在气流方向上具有平背型翼的后缘(10c)。空气动力元件(10)还包括连接在所述空气动力元件(10)的后缘(10c)上的非对称燕尾形腔体(1，2)。所述空气动力元件(10)为例如应用在风力涡轮机的转子叶片中。
摘要（英）：

Aerodynamic element having a cross section in an airflow direction with a trailing edge (10c). The aerodynamic element (10) further comprises a non-symmetrical swallow tail shaped cavity body (1, 2) attached to the trailing edge (10c) of the aerodynamic element (10).The aerodynamic element (10) is e.g. applied in a rotor blade for a wind turbine.

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