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Characterizing Influence of Transition to Turbulence on the Propulsive Performance of Underwater Gliders

机译:表征湍流过渡对水下滑翔机推进性能的影响

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Two models of underwater gliders were tested in a wind tunnel: one corresponding to a legacy shape commonly used in contemporary vehicles and the other a scaled down version of a new design. Performance of the two vehicles was characterized over a range of speeds and angles of attack. Particular attention was paid to the effect of sharp features along the hulls of the two vehicles and how they affect the observed flow regime. It has been shown that the new design, which uses a bow shape designed to encourage natural laminar flow, benefits from a 10% reduction of parasitic drag and 13% increase in lift-to-drag when the hull surface is smooth. The legacy glider, made up of a faired bow and a cylindrical hull, suffers from laminar separation and up to 100% increase in induced drag if the flow over its bow is prevented from transitioning to a turbulent state before encountering adverse pressure gradient at lower Reynolds numbers. This results in lowering of attainable speed at shallow glide path angles, whereas the associated parasitic drag reduction is demonstrated to increase the maximum velocity of the glider when moving at glide slopes greater than approximately 30 degrees.
机译:在风洞中测试了两种型号的水下滑翔机:一种对应于现代车辆中常用的传统形状,另一种则是新设计的缩小版本。在速度和迎角范围内对这两种车辆的性能进行了表征。特别注意了沿两辆车的船体的尖锐特征的影响以及它们如何影响观察到的流动状态。研究表明,船体表面光滑时,采用弓形设计以鼓励自然层流的新设计可将寄生阻力降低10%,将举升阻力提高13%,从而受益。传统的滑翔机由流线型船首和圆柱形船体组成,如果在较低的雷诺兹遇到不利的压力梯度之前,防止其船首上的气流过渡到湍流状态,则会遭受层流分离并导致阻力增加多达100%。数字。这会导致在较浅的滑行路径角处降低可达到的速度,而在滑行坡度大于约30度时,相关的寄生阻力减小可提高滑行机的最大速度。

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