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首页> 外文期刊>Revista Brasileira de Engenharia Agricola e Ambiental >AN EXPERIMENTAL STUDY ON WINGTIP DEVICES FOR AGRICULTURAL AIRCRAFT
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AN EXPERIMENTAL STUDY ON WINGTIP DEVICES FOR AGRICULTURAL AIRCRAFT

机译:农机翼梢装置的实验研究。

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The induced drag in an aircraft be reduced through modifications of the wing tip. Some models displace wingtips vortices outwards diminishing the induced drag. Concerning agricultural airplanes, wing tip vortex position is really important while spreading products over a plantation. In this work, wind tunnel tests were made in order to study the influence in aerodynamic characteristics and vortex position over Brazilian agricultural aircraft, by the following types of wing tips: delta tip, winglet and down curved. The down curved tip was better for total drag reduction but not good with reference to vortex position. The delta tip gave moderate improvement on aerodynamic characteristic but a good vortex position. The winglet had a better vortex position but caused an undesirable result with reference to the wing root bending moment. Therefore, delta tip is more promising for agricultural aircraft.
机译:通过修改翼尖可以减少飞机上的感应阻力。一些模型向外移动翼尖涡流,以减小感应阻力。对于农用飞机,在将产品散布到人工林中时,翼尖涡旋位置确实很重要。在这项工作中,通过以下类型的翼尖进行了风洞试验,以研究空气动力学特性和涡流位置对巴西农用飞机的影响:三角翼尖,小翼和向下弯曲。向下弯曲的尖端可降低总阻力,但相对于涡旋位置则不好。三角形尖端使空气动力学特性得到了适度改善,但涡流位置良好。小翼具有更好的涡旋位置,但相对于翼根弯曲力矩却产生了不良结果。因此,三角翼尖端对于农机而言更有希望。

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