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Aerodynamic design analysis of a UAV for superficial research of volcanic environments

机译:用于火山环境浅层研究的无人机空气动力学设计分析

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When volcanoes manifest unusual signs of activity, real-time data aids for evaluating and communicating reports about volcanic hazards. For this reason, the present research aims the aerodynamic design of a low-cost unmanned aerial vehicle (UAV) able to perform aerial surveillance of volcanic environments. Its main mission is to transmit real-time volcanic data to a remote location, in order to aid to forecast volcanic eruptions, as well as avoiding the exposition of pilots and scientists to these dangerous flight conditions. During the conceptual design phase, classical and new design procedures were developed in order to determine the vehicle design requirements, in relation to its flight in a hard scenario like an active volcano. Likewise, the main geometric, aerodynamic, stability and performance parameters of the UAV were calculated and assessed through theoretical analytical presizing and Computer-aided Design (CAD) methods. After obtaining the final concept, the aerodynamic design was carried out considering the constraints found in the previous design phase. In this way, an accurate estimation of the aerodynamic coefficients was developed, through analytical simulations, Computational Fluid Dynamics (CFD) simulations and wind tunnel testing. Results showed that the entire design process was consistent because the analytical, numerical and experimental results were greatly similar in the Lift (C-L) and Drag (C-D) coefficients. Furthermore, the UAV characteristics are within the limits of the design requirements, presenting several aerodynamic and performance advantages in comparison to other vehicles used in the same mission. This suggested that, on a large scale, the aerodynamic behavior of the UAV is suitable for performing the mission for which it was created. However, actual-environmental studies are still necessary in order to validate the reliability of the designed UAV. (C) 2017 Elsevier Masson SAS. All rights reserved.
机译:当火山显示异常活动迹象时,实时数据可帮助评估和传达有关火山危害的报告。由于这个原因,本研究的目标是能够对火山环境进行空中监视的低成本无人机(UAV)的空气动力学设计。其主要任务是将实时火山数据传输到远程位置,以帮助预测火山喷发,并避免将飞行员和科学家暴露在这些危险的飞行条件下。在概念设计阶段,开发了经典和新的设计程序来确定车辆设计要求,以应对其在诸如活火山之类的艰难情况下的飞行情况。同样,无人机的主要几何,空气动力学,稳定性和性能参数是通过理论上的分析尺寸和计算机辅助设计(CAD)方法计算和评估的。在获得最终概念后,考虑了在先前设计阶段中发现的约束条件,进行了空气动力学设计。通过分析模拟,计算流体动力学(CFD)模拟和风洞测试,以这种方式开发了对空气动力学系数的精确估计。结果表明,整个设计过程是一致的,因为在升力(C-L)和阻力(C-D)系数方面的分析,数值和实验结果非常相似。此外,无人机特性在设计要求的范围内,与同一任务中使用的其他车辆相比,具有几项空气动力学和性能优势。这表明,在很大程度上,无人机的空气动力学行为适合执行其创建的任务。但是,为了验证所设计的无人机的可靠性,仍然需要进行实际环境研究。 (C)2017 Elsevier Masson SAS。版权所有。

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