无人机叶片的 CFD 分析

Rajendra Ghatode, Nitanshu Modekar, Harsh Bode, Siddharrh Lakhwani
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引用次数: 0

摘要

无人机技术在摄影、军事、运输、体育等各个领域和应用中都得到了快速发展。因此,每种无人机的设计都需要不同的空气动力学要求,其中包括不同类型的螺旋桨设计。螺旋桨通过旋转和产生气流,为无人机或无人驾驶飞行器(UAV)提供升力或推力。本文对不同螺旋桨的气动性能和声学特征进行了新颖的综合研究,重点关注叶片扭转角效应。本文使用 CATIA V5 和计算流体动力学(CFD)模拟进行设计,以检查和比较不同形状的无人机螺旋桨的气动性能、阻力和升力。因此,这项工作的重点是研究不同无人机叶片的空气动力效应。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
CFD Analysis of Drone Blade
Drone technology is seen to be rapidly advancing in various fields and applications including photography, military, transportation, sports, and many more. Therefore, each drone design requires different aerodynamic requirements, which includes different types of propeller designs. By revolving and generating airflow, the propellers give drones or unmanned aerial vehicles (UAV) a lift force or thrust. This paper presents a novel integrated study of the aerodynamic performance and acoustic signature of different propellers with a specific focus on the blade twist angle effect. Designed using CATIA V5 and computational fluid dynamic (CFD) simulations were utilized to examine and compare the aerodynamic performance, Drag and Lift between different shapes of the drone propellers. Therefore, this work falls on the study of the aerodynamic effect of different drone blades
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