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Sustained drag reduction in a turbulent flow using a low-temperature Leidenfrost surface

机译:使用低温莱顿弗罗斯特表面在湍流中实现持续减阻

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摘要

Skin friction drag contributes a major portion of the total drag for small and large water vehicles at high Reynolds number (Re). One emerging approach to reducing drag is to use superhydrophobic surfaces to promote slip boundary conditions. However, the air layer or “plastron” trapped on submerged superhydrophobic surfaces often diminishes quickly under hydrostatic pressure and/or turbulent pressure fluctuations. We use active heating on a superhydrophobic surface to establish a stable vapor layer or “Leidenfrost” state at a relatively low superheat temperature. The continuous film of water vapor lubricates the interface, and the resulting slip boundary condition leads to skin friction drag reduction on the inner rotor of a custom Taylor-Couette apparatus. We find that skin friction can be reduced by 80 to 90% relative to an unheated superhydrophobic surface for Re in the range 26,100 ≤ Re ≤ 52,000. We derive a boundary layer and slip theory to describe the hydrodynamics in the system and show that the plastron thickness is h = 44 ± 11 μm, in agreement with expectations for a Leidenfrost surface.
机译:对于雷诺数(Re)高的小型和大型水上车辆,皮肤摩擦阻力在总阻力中占很大比例。减少阻力的一种新兴方法是使用超疏水表面来促进滑移边界条件。但是,在静水压力和/或湍流压力波动下,滞留在淹没的超疏水表面上的空气层或“ plastron”通常会迅速减少。我们在超疏水的表面上使用主动加热,以在相对较低的过热温度下建立稳定的蒸汽层或“ Leidenfrost”状态。连续的水蒸气薄膜润滑了界面,产生的滑移边界条件导致定制泰勒-库埃特装置的内转子上的皮肤摩擦阻力减小。我们发现,相对于未经加热的超疏水表面,Re在26,100≤Re≤52,000范围内,皮肤摩擦可以降低80%至90%。我们推导了边界层和滑移理论来描述系统中的流体动力学,并表明the板厚度为h = 44±11μm,与对莱顿弗罗斯特表面的期望相符。

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