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Wing tail of a wing and a wing with such wing tail

机译:机翼的机翼尾翼和带有这种机翼尾翼的机翼

摘要

Wing tail (W; W1, W2, W4, W5, W6, W7, W8) for a wing (T; 10a, 10b) having an inner end (E1) and an outer end (E2) and having the local V Angle of the wing tail (W; W1, W2, W4, W5, W6, W7, W8) increases or decreases from the inner end (E1) to the outer end (E2), with a pressure-side flow surface (UW) and a suction-side flow surface (E). PW), wherein at the wing tail (W; W1, W2, W4, W5, W6, W7, W8) at least two are each defined from the flow surface of the wing tail (W; W1, W2, W4, W5, W6, W7, W8) additional wing pieces (100, 101, 102, 103) are arranged, and wherein the additional wing pieces (100, 101, 102, 103) are connected to the surface of the wing tail (W; W1, W2, W4, W5, W6, W7, W8) each form a cut surface (q0) separated from each other and airfoils (T) having such a wing tail (W; W1, W2, W4, W5, W6, W7, W8).
机译:机翼(T; 10a,10b)的机翼尾翼(W; W1,W2,W4,W5,W6,W7,W8),其内端(E1)和外端(E2)且局部V角为机翼尾翼(W; W1,W2,W4,W5,W6,W7,W8)从内端(E1)到外端(E2)增大或减小,并带有压力侧流动面(UW)和吸入侧流动表面(E)。 PW),其中在机翼尾翼(W; W1,W2,W4,W5,W6,W7,W8)从机翼尾翼(W; W1,W2,W4,W5, W6,W7,W8)布置有附加的翼片(100、101、102、103),其中,附加的翼片(100、101、102、103)连接至机翼尾翼(W; W1, W2,W4,W5,W6,W7,W8)分别形成彼此分开的切面(q0)和具有这种机翼尾翼(W; W1,W2,W4,W5,W6,W7,W8的机翼(T)) )。

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