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An experimental study into the effect of transitional flow on the performance of underwater glider wings

机译:一种实验研究转型流动对水下滑翔机翼性能的影响

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The experimental procedures developed to measure small forces generated by underwater vehicle appendages in a wind tunnel are described. These involve using precision load cell sensors arranged into a bespoke dynamometer, that has been integrated into a stand-alone wind tunnel rig. The set up is used to quantify performance of a scaled underwater glider hydrofoil, with particular care being paid to the effects of laminar and transitional flow features. Present data are benchmarked against similar measurements and simulations and it is shown that satisfactory results may be obtained with the current approach despite its simplicity and low cost. The apparatus is then used to show that the presence of laminar flow significantly affects performance of the considered foil at Reynolds numbers corresponding to a typical regime in which underwater gliders operate.
机译:描述了用于测量风隧道中的水下车辆附件产生的小力的实验程序。这些涉及使用布置成定制测功机的精密载荷电池传感器,该传感器已集成到独立的风洞钻机中。该设置用于量化缩放水下滑翔机水翼的性能,特别注意层流和过渡流动特征的效果。目前的数据是针对类似的测量和模拟的基准测试,并且表明尽管其简单性和低成本,但是当前方法可以获得令人满意的结果。然后,该装置表明层流的存在显着地影响了与水下滑翔机操作的典型制度对应的雷诺数的所考虑的箔的性能。

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