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Investigating the Autorotational Performance of Scaled Samara Rotor in Vertical and Forward Flight

机译:研究定标萨马拉转子在垂直和向前飞行中的自转性能

摘要

Samara seeds are nature’s most efficient fliers, they can create twice the lift compared to translating wings by the creation of the Leading edge vortex (LEV). Realising this, numerous Samara inspired UAVs are being created. However, a number of research questions still need to be answered to be able to harness the benefit of the LEV for UAV applications. In particular, if scaling up the natural Samara degrades its aerodynamics performance and how well the scaled Samara wings perform in autorotation in both the forward and vertical flight regimes. This paper explores the effects of scaling by a series of drop tests and wind tunnel tests. It was found that the vertical aerodynamic performance of the Samara wing starts degrading as its scale reaches a ratio of 8:1 size to the natural Samara seed. In terms of forward flight, the natural Samara found it hard to cope with any slight deviations from vertical descent whereas the artificial scaled Samara were able to autorotate up to 80 degrees shaft angle relative to the wind direction. The effect of scaling in forward flight was also explored; a 1:1 to 4:1 scaling boosted the thrust by around seven folds whereas a 4:1 to 8:1 scaling increased the thrust by only around four times.
机译:萨马拉种子是大自然中最高效的飞行物,通过创建前缘涡流(LEV),与平移机翼相比,它们可以产生两倍的升力。意识到这一点,许多萨马拉启发了无人机。但是,仍然需要回答许多研究问题,才能利用LEV在无人机应用中的优势。特别地,如果按比例放大天然翼果会降低其空气动力学性能,并且按比例缩放的翼果机翼在前向和垂直飞行状态下的自转性能如何。本文通过一系列跌落测试和风洞测试来探讨结垢的影响。发现萨马拉翼的垂直空气动力学性能随着其规模与天然萨马拉种子的比例达到8:1而开始下降。在向前飞行方面,天然萨马拉发现很难应对垂直下降的任何细微偏差,而人造鳞片萨马拉能够相对于风向自动旋转高达80度的轴角。还探讨了前向飞行中缩放的影响; 1:1到4:1的缩放比例将推力提高了约7倍,而4:1到8:1的缩放比例则仅将推力提高了约四倍。

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