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Adhesive panels of microvane arrays for reducing effects of wingtip vortices
Adhesive panels of microvane arrays for reducing effects of wingtip vortices
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机译:微叶片阵列的粘合板,用于降低翼尖涡流的影响
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摘要
In one embodiment, a wing includes a low pressure side, a high pressure side opposite the low pressure side, and a drag reducing apparatus coupled to the low pressure using an adhesive. The drag reducing apparatus includes a first side coupled to the low pressure side of the wing, and a second side opposite the first side, the second side comprising a plurality of vortex generators arranged in an array configuration, the array configuration of vortex generators operable to weaken a wingtip vortex generated by the wing by generating one or more vane vortices near an end of the low pressure side of the wing.
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