Comprehensive computational investigations on various aerospace materials under complicated loading conditions through conventional and advanced analyses: a verified examination
نویسندگان
چکیده
Most failures develop as a result of lack resistivity information at the internal structure level during typical loading situations such shock load and impact load. Impact loads have significant on component’s structural performance. A careful, organized examination settings their side effects can reveal how well something withstand peak loads. First, this study investigated analyses nine varied lightweight composite materials through conventional experimental setup computational tools. So, best three are shortlisted for further investigation under complicated explicit analysis. Second, behavior subjected to rapid circumstances in several real-time applications. The applications chosen include bullet crash analysis, unmanned aerial vehicle (UAV) propellers, car bumpers. different principal composites, carbon fiber-reinforced polymer (CFRP), glass (GFRP), Kevlar (KFRP), selected applied analysis using ANSYS Workbench’s technique-based finite element (FEA). comparison assessments conducted stumpy characteristics stress equivalent strain. Two distinct grid convergence tests were performed check whether processes discretization correct. standard methodologies used all applications, resulting error percentages that within acceptable bounds, ensuring generation dependable outputs. ideal material is fiber-based with minimal defect affectability types Furthermore, multidisciplinary optimizations performed, KFRP verified give good resistance reduced dense contribution.
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ژورنال
عنوان ژورنال: Frontiers in Materials
سال: 2023
ISSN: ['2296-8016']
DOI: https://doi.org/10.3389/fmats.2023.1147310