Enhancing the Photophoretic Lift Force at Low Reynolds Numbers using Three-Dimensional Porous Structures

Thomas J. Celenza, Zhipeng Lu, Matthew Campbell, Mohsen Azadi, I. Bargatin
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Abstract

It is well documented that the lift force of hovering micro aerial vehicles can be enhanced by increasing their air-flow velocities. This is commonly accomplished using nozzles and other flow-manipulating geometries with Reynolds numbers above order 100. [1,2] However, the effects of nozzles and other geometries are not well characterized for lower Reynolds numbers within the Stokes’ regime. In general, controlled flight in low-Reynolds number conditions using conventional propulsion methods such as propellers is difficult. Instead, levitation at ultra-low Reynolds number conditions has been accomplished through other means, including photophoretically as demonstrated recently by Cortes et al. [3] and Azadi et al. [4]. These works levitated planar materials without macroscale geometric enhancements and relied strictly on the lift force created through a temperature or accommodation coefficient difference across the planar structure. In the current work, we numerically explored the feasibility of multi-scale structures operating at low-to-moderate Reynolds numbers that pair microscale photophoretic gas pumping with macroscale jet-inducing nozzles. We used ANSYS Fluent to simulate the lift forces in centimeter-scale porous membrane discs (no macroscale enhancements) and in conical nozzles created from porous membranes. Our results indicate that porous conical nozzles provide an order of magnitude lift enhancement relative to flat discs with inlet velocities as low as 10-6 m/s. In addition, we developed a semi-analytical flow model and found good agreement with the simulations. We are currently fabricating mylar structures analogous to the simulation geometries, laser machined to create porosity and adhered to lightweight frames to maintain their shape. The multi-scale structures we create will be of critical importance for exploring low-pressure environments such as Earth’s mesosphere and the Martian atmosphere. References: [1] Benedict, Moble, et al. "Experimental investigation of micro air vehicle scale helicopter rotor in hover." International Journal of Micro Air Vehicles3 (2015): 231-255. [2] Seddon, John M., and Simon Newman. Basic helicopter aerodynamics. Vol. 40. John Wiley & Sons, 2011. [3] Cortes, John, et al. "Photophoretic levitation of macroscopic nanocardboard plates." Advanced Materials16 (2020): 1906878. [4] Azadi, Mohsen, et al. "Controlled levitation of nanostructured thin films for sun-powered near-space flight." Science Advances7 (2021): eabe1127.
利用三维多孔结构增强低雷诺数下的光致升力
有充分的文献证明,悬停微型飞行器的升力可以通过增加其气流速度来增强。这通常是通过使用雷诺数在100阶以上的喷嘴和其他控制流动的几何形状来实现的。[1,2]然而,对于Stokes区域内的较低雷诺数,喷嘴和其他几何形状的影响并没有很好地表征。一般来说,在低雷诺数条件下,使用传统的推进方法(如螺旋桨)进行控制飞行是困难的。相反,超低雷诺数条件下的悬浮可以通过其他方式实现,包括最近由Cortes等人[3]和Azadi等人[4]证明的光致悬浮。这些工程使平面材料悬浮,没有宏观几何增强,并严格依赖于通过平面结构的温度或调节系数差异产生的升力。在目前的工作中,我们在数值上探索了在中低雷诺数下运行的多尺度结构的可行性,该结构将微尺度光致气体泵送与宏观尺度射流诱导喷嘴配对。我们使用ANSYS Fluent模拟了厘米尺度多孔膜盘(没有宏观尺度的增强)和由多孔膜制成的锥形喷嘴中的升力。我们的研究结果表明,当进口速度低至10-6 m/s时,多孔锥形喷嘴相对于平盘喷嘴提供了一个数量级的升力增强。此外,我们建立了一个半解析的流动模型,与模拟结果吻合良好。我们目前正在制造类似于模拟几何形状的聚酯膜结构,激光加工以产生孔隙,并粘附在轻质框架上以保持其形状。我们创造的多尺度结构对于探索地球中间层和火星大气层等低压环境至关重要。参考文献:[1]Benedict, Moble等。微型飞行器级直升机旋翼悬停试验研究。国际微型飞行器学报(2015):231-255。[2]约翰·M·塞登,西蒙·纽曼。基本的直升机空气动力学。40卷。。John Wiley & Sons, 2011。[3]刘志强,刘志强,等。宏观纳米纸板的光致悬浮。材料工程学报,2016,37(2):389 - 389。[4]张晓明,张晓明。“用于太阳能近太空飞行的纳米结构薄膜的控制悬浮。”科学进展7 (2021):eabe1127。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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