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Aircraft wing with high swept back leading edge, particulary delta wing
Aircraft wing with high swept back leading edge, particulary delta wing
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机译:具有高后掠边缘的飞机机翼,特别是三角翼
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摘要
The aircraft wing (3) has sharply swept-back leading edges (7). A conical vortex forms on the suction side (5) when air flows over the wing. There is at least one guide surface (11) for this vortex, forming an angle ( delta ) to the normal to the aircraft's longitudinal axis (2) of not more than 85 degrees . The guide surface runs parallel to the axis (12) of the conical vortex and between it and the leading edge.
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