Multi-perspective structural integrity-based computational investigations on airframe of Gyrodyne-configured multi-rotor UAV through coupled CFD and FEA approaches for various lightweight sandwich composites and alloys

IF 3.6 4区 材料科学 Q2 MATERIALS SCIENCE, MULTIDISCIPLINARY
Selvaramanan Vijayalakshmi, Aravindha Vasan Sekar, Ahmed Mohamed Hassan, Beena Stanislaus Arputharaj, Shyam Sundar Jayakumar, Hussein A. Z. AL-bonsrulah, Parvathy Rajendran, Senthil Kumar Madasamy, Arunkumar Karuppasamy, Vijayanandh Raja
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Abstract

As this unmanned aerial vehicle (UAV) has a planned airframe that can carry a 25 kg payload, understanding its structural capabilities, such as its compressive and tensile strengths under different situations, is essential. For the purpose of comprehending the fluid–structure interaction (FSI) of the fuselage, this study designs and analyses the lightweight materials used in the airframe of a complex Gyrodyne UAV. A computer model of a composite airframe for a Gyrodyne UAV is built to examine its durability. An essential factor in the aircraft business is minimizing unnecessary weight, and this FSI study emphasizes the importance of sandwiches and their hybrid combinations in this regard. After the material finalization, around 140 material combinations are tested using an advanced computational composite platform, in which four different lightweight material families are implemented. The fluid load (pressure) is imported into ANSYS workbench 17.2, and the structural airframe is then solved according to the boundary conditions of the application domain. Also, experimental experiments using the high-speed jet facility are run to verify computational improvements. Materials for the airframe of the Gyrodyne UAV have been narrowed down to a final list of contenders. As the work focuses on the FSI analysis, not much computational fluid dynamics (CFD) results were discussed here. Only the imported pressure from the CFD analysis was imposed on to the Gyrodyne UAV to proceed for the FSI analysis.
通过对各种轻质夹层复合材料和合金的 CFD 和 FEA 耦合方法,对陀螺仪配置的多旋翼无人机机身进行基于结构完整性的多视角计算研究
由于这种无人驾驶飞行器(UAV)的计划机身可承载 25 公斤的有效载荷,因此了解其结构能力(如在不同情况下的抗压和抗拉强度)至关重要。为了理解机身的流固相互作用(FSI),本研究设计并分析了用于复杂陀螺仪无人机机身的轻质材料。还建立了一个陀螺仪无人机复合材料机身的计算机模型,以检验其耐用性。飞机业务中的一个重要因素是最大限度地减少不必要的重量,FSI 的这项研究强调了三明治及其混合组合在这方面的重要性。材料确定后,使用先进的计算复合材料平台对大约 140 种材料组合进行了测试,其中使用了四种不同的轻质材料系列。流体载荷(压力)被导入 ANSYS workbench 17.2,然后根据应用领域的边界条件对结构机身进行求解。此外,还使用高速喷气设施进行了实验,以验证计算的改进。陀螺仪无人机的机身材料已缩小到最后的竞争者名单。由于工作重点是 FSI 分析,因此这里讨论的计算流体动力学 (CFD) 结果不多。只有将 CFD 分析得出的输入压力施加到 Gyrodyne 无人机上,才能进行 FSI 分析。
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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来源期刊
Reviews on Advanced Materials Science
Reviews on Advanced Materials Science 工程技术-材料科学:综合
CiteScore
5.10
自引率
11.10%
发文量
43
审稿时长
3.5 months
期刊介绍: Reviews on Advanced Materials Science is a fully peer-reviewed, open access, electronic journal that publishes significant, original and relevant works in the area of theoretical and experimental studies of advanced materials. The journal provides the readers with free, instant, and permanent access to all content worldwide; and the authors with extensive promotion of published articles, long-time preservation, language-correction services, no space constraints and immediate publication. Reviews on Advanced Materials Science is listed inter alia by Clarivate Analytics (formerly Thomson Reuters) - Current Contents/Physical, Chemical, and Earth Sciences (CC/PC&ES), JCR and SCIE. Our standard policy requires each paper to be reviewed by at least two Referees and the peer-review process is single-blind.
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