首页> 外文会议>Congress of the International Council of the Aeronautical Sciences;ICAS 2008 >SINGLE VERSUS MULTIPLE WINGLETS: NUMERICAL AND EXPERIMENTAL INVESTIGATION
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SINGLE VERSUS MULTIPLE WINGLETS: NUMERICAL AND EXPERIMENTAL INVESTIGATION

机译:单支多小翼:数值和实验研究

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The main goal of the proposed paper is the numerical and experimental investigation of multiple winglets influence on the reduction of induced drag. This results in the improvement of climbing performances of a motorglider or hang-glider. In a precedent work [1] a set of multiple winglets, very similar to the bird tip feathers called remiges, were designed and optimized for the hang-glider belonging to Angelo D'Arrigo, a world champion hang-glider pilot and record holder. The research aims was to optimize the CL~(1,5)/CD parameter since this is directly proportional to the sink rate. In this work the effects of the multiple winglets, set on an elliptical wing and tested in a wind tunnel, are compared to the effects of three different single 'classical' winglets that were designed using a panel method code and were also tested in the same wind tunnel in order to compare their span efficiency to the one of the multiple winglets.
机译:拟议论文的主要目的是对多个小翼对减小诱导阻力的影响进行数值和实验研究。这导致了电动滑翔机或悬挂式滑翔机的爬坡性能的改善。在先例[1]中,为世界滑翔机飞行员兼记录保持者Angelo D'Arrigo的滑翔机设计并优化了一组与翼尖羽毛非常相似的复式小翼。研究目的是优化CL〜(1,5)/ CD参数,因为它与吸收速率直接成正比。在这项工作中,将设置在椭圆形机翼上并在风洞中测试的多个小翼的效果与使用面板方法代码设计并在相同的条件下进行测试的三个不同的“经典”小翼的效果进行了比较。风洞,以便将其跨度效率与多个小翼之一进行比较。

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