{"title":"Analysis of Residual Post-Impact Compressive Strength of Composite Laminates Under Hygrothermal Conditions","authors":"Yue Guan, Shi Yan, Xixi Chen, Yuxuan Zhang, Xin Wang, Hanhua Li, Yun Zhao, Junjun Zhai","doi":"10.1007/s10443-024-10258-5","DOIUrl":null,"url":null,"abstract":"<p>This paper is a continuation study of the residual compressive strength of composite laminates after impact under hygrothermal conditions. Two carbon fibre/epoxy plywood specimens with different lay-ups ([45/-45/0/0/45/0/0/0/90/-45/0]s and [45/-45/0/90/0 /0/0/0/90/0/-45/45]s) were investigated, The materials were subjected to 500 h, 1000 h and 2000 h of service time in a climatic chamber at a temperature of 60 °C and 100% relative humidity, followed by low-velocity post-impact compression using an energy level of 15 J. Experimental and numerical simulations are used to study the residual compressive strength and damage extension of the material. Using the ultrasonic C-scan technique, the internal damage of the specimens was scanned, and the damage evolution in impact and compression tests was analysed. Damage evolution in impact and compression tests was investigated using ultrasonic C-scanning to scan the internal damage of the specimens. The strain change maps of the specimens during compression are studied using the Digital Imaging (DIC) technique. Vumat subroutine coded in Fortran and used in commercial software (ABAQUS) for numerical simulation. To study the effect of damage extension of materials on post-impact and post-impact compression for different hygrothermal times. It was found that the residual compressive strength depended on factors such as the material's hygrothermal time and the initial defects in the plywood; that the 90° and ± 45° fibre orientations played a positive role in the material's hygrothermal; that the hygrothermal made the material's damage more catastrophic; and that the buckling of hygrothermal specimens was not only at the impact position, but was also reflected at the edges. In CAI testing, it was found that the hygrothermally treated specimens were damaged similarly to the desiccation treated specimens, but that compression resulted in a flexural position affected by hygrothermal, which determined the material CAI strength. </p>","PeriodicalId":468,"journal":{"name":"Applied Composite Materials","volume":"158 1","pages":""},"PeriodicalIF":2.3000,"publicationDate":"2024-08-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Applied Composite Materials","FirstCategoryId":"88","ListUrlMain":"https://doi.org/10.1007/s10443-024-10258-5","RegionNum":4,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"MATERIALS SCIENCE, COMPOSITES","Score":null,"Total":0}
引用次数: 0
Abstract
This paper is a continuation study of the residual compressive strength of composite laminates after impact under hygrothermal conditions. Two carbon fibre/epoxy plywood specimens with different lay-ups ([45/-45/0/0/45/0/0/0/90/-45/0]s and [45/-45/0/90/0 /0/0/0/90/0/-45/45]s) were investigated, The materials were subjected to 500 h, 1000 h and 2000 h of service time in a climatic chamber at a temperature of 60 °C and 100% relative humidity, followed by low-velocity post-impact compression using an energy level of 15 J. Experimental and numerical simulations are used to study the residual compressive strength and damage extension of the material. Using the ultrasonic C-scan technique, the internal damage of the specimens was scanned, and the damage evolution in impact and compression tests was analysed. Damage evolution in impact and compression tests was investigated using ultrasonic C-scanning to scan the internal damage of the specimens. The strain change maps of the specimens during compression are studied using the Digital Imaging (DIC) technique. Vumat subroutine coded in Fortran and used in commercial software (ABAQUS) for numerical simulation. To study the effect of damage extension of materials on post-impact and post-impact compression for different hygrothermal times. It was found that the residual compressive strength depended on factors such as the material's hygrothermal time and the initial defects in the plywood; that the 90° and ± 45° fibre orientations played a positive role in the material's hygrothermal; that the hygrothermal made the material's damage more catastrophic; and that the buckling of hygrothermal specimens was not only at the impact position, but was also reflected at the edges. In CAI testing, it was found that the hygrothermally treated specimens were damaged similarly to the desiccation treated specimens, but that compression resulted in a flexural position affected by hygrothermal, which determined the material CAI strength.
本文继续研究了复合材料层压板在湿热条件下受到冲击后的残余抗压强度。研究了两种不同层叠结构的碳纤维/环氧胶合板试样([45/-45/0/0/45/0/0/0/90/-45/0]s和[45/-45/0/90/0/0/0/90/0/45/45]s),分别在温度为60 °C、相对湿度为100%的气候箱中使用500小时、1000小时和2000小时,然后使用15 J的能量水平进行低速冲击后压缩。实验和数值模拟用于研究材料的残余抗压强度和损伤扩展。利用超声波 C 扫描技术扫描了试样的内部损伤,并分析了冲击和压缩试验中的损伤演变。利用超声波 C 扫描技术扫描试样的内部损伤,研究了冲击和压缩试验中的损伤演变。使用数字成像(DIC)技术研究了压缩过程中试样的应变变化图。Vumat 子程序采用 Fortran 编码,并在商业软件 (ABAQUS) 中用于数值模拟。研究不同湿热时间下材料的损伤扩展对冲击后和冲击后压缩的影响。结果发现,残余抗压强度取决于材料的湿热时间和胶合板的初始缺陷等因素;90°和± 45°纤维取向对材料的湿热起积极作用;湿热使材料的损伤更具灾难性;湿热试样的屈曲不仅在冲击位置,而且在边缘也有体现。在 CAI 试验中发现,湿热处理试样的损坏情况与干燥处理试样类似,但压缩导致的弯曲位置受到湿热的影响,这决定了材料的 CAI 强度。
期刊介绍:
Applied Composite Materials is an international journal dedicated to the publication of original full-length papers, review articles and short communications of the highest quality that advance the development and application of engineering composite materials. Its articles identify problems that limit the performance and reliability of the composite material and composite part; and propose solutions that lead to innovation in design and the successful exploitation and commercialization of composite materials across the widest spectrum of engineering uses. The main focus is on the quantitative descriptions of material systems and processing routes.
Coverage includes management of time-dependent changes in microscopic and macroscopic structure and its exploitation from the material''s conception through to its eventual obsolescence.