Domínguez-Pumar Manuel, Kowalski Lukasz, Jiménez Vicente, Rodríguez Ivette, Soria Manel, Bermejo Sandra, Pons-Nin Joan
Micro and Nano Technologies Group, Electronic Engineering Department, Universitat Politècnica de Catalunya, 08034 Barcelona, Spain.
Turbulence and Aerodynamics in Mechanical and Aerospace Engineering Research Group, Universitat Politècnica de Catalunya, 08222 Terrassa, Spain.
Sensors (Basel). 2020 Oct 20;20(20):5912. doi: 10.3390/s20205912.
This paper analyzes the behavior of a miniature 3D wind sensor designed for Mars atmosphere. The sensor is a spherical structure of 10 mm diameter divided in four sectors. By setting all the sectors to constant temperature, above that of the air, the 3D wind velocity vector can be measured. Two sets of experiments have been performed. First, an experimental campaign made under typical Mars conditions at the Aarhus Wind Tunnel Simulator is presented. The results demonstrate that both wind speed and angle can be efficiently measured, using a simple inverse algorithm. The effect of sudden wind changes is also analyzed and fast response times in the range of 0.7 s are obtained. The second set of experiments is focused on analyzing the performance of the sensor under extreme Martian wind conditions, reaching and going beyond the Dust Devil scale. To this purpose, both high-fidelity numerical simulations of fluid dynamics and heat transfer and experiments with the sensor have been performed. The results of the experiments, made for winds in the Reynolds number 1000-2000 range, which represent 65-130 m/s of wind speed under typical Mars conditions, further confirm the simulation predictions and show that it will be possible to successfully measure wind speed and direction even under these extreme regimes.
本文分析了一种为火星大气设计的微型三维风传感器的性能。该传感器是一个直径为10毫米的球形结构,分为四个扇区。通过将所有扇区设置为高于空气温度的恒定温度,可以测量三维风速矢量。进行了两组实验。首先,介绍了在奥胡斯风洞模拟器的典型火星条件下开展的一系列实验。结果表明,使用简单的反演算法可以有效地测量风速和风向。还分析了风速突然变化的影响,并获得了0.7秒范围内的快速响应时间。第二组实验重点分析了该传感器在极端火星风条件下的性能,该条件达到并超过了尘卷风规模。为此,进行了流体动力学和传热的高保真数值模拟以及传感器实验。在雷诺数1000 - 2000范围内进行的实验结果,代表了典型火星条件下65 - 130米/秒的风速,进一步证实了模拟预测,并表明即使在这些极端条件下也能够成功测量风速和风向。