{"title":"循环载荷下无卷曲织物复合材料损伤演化与刚度退化的综合数字成像技术","authors":"Erli Shi, John Montesano","doi":"10.1016/j.compstruct.2025.119513","DOIUrl":null,"url":null,"abstract":"<div><div>A novel integrated digital imaging technique was developed to automatically characterize damage and simultaneously monitor stiffness degradation in non-crimp fabric glass fiber/reactive thermoplastic cross-ply laminates subject to tension–tension cyclic loading. Under a peak stress of 50 % UTS, the laminate exhibited four distinct stages of stiffness degradation, including a significant drop during the first cycle due to 90° fiber tow crack initiation, a gradual decrease due to crack multiplication and propagation up to saturation, a stable phase comprising localized delamination crack propagation, and a sudden drop prior to specimen failure. Under a peak stress of 75 % UTS, both 0° and 90° fiber tow cracks developed during the first stage followed by an accelerated growth rate and reduced 90° tow crack density at saturation. The integrated digital imaging technique proved to effectively correlate damage events with stiffness degradation, leading to a deeper understanding of the fatigue behavior of glass fiber/thermoplastic composites.</div></div>","PeriodicalId":281,"journal":{"name":"Composite Structures","volume":"371 ","pages":"Article 119513"},"PeriodicalIF":7.1000,"publicationDate":"2025-07-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Integrated digital imaging technique for correlation of damage evolution and stiffness degradation in non-crimp fabric composite materials under cyclic loading\",\"authors\":\"Erli Shi, John Montesano\",\"doi\":\"10.1016/j.compstruct.2025.119513\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>A novel integrated digital imaging technique was developed to automatically characterize damage and simultaneously monitor stiffness degradation in non-crimp fabric glass fiber/reactive thermoplastic cross-ply laminates subject to tension–tension cyclic loading. Under a peak stress of 50 % UTS, the laminate exhibited four distinct stages of stiffness degradation, including a significant drop during the first cycle due to 90° fiber tow crack initiation, a gradual decrease due to crack multiplication and propagation up to saturation, a stable phase comprising localized delamination crack propagation, and a sudden drop prior to specimen failure. Under a peak stress of 75 % UTS, both 0° and 90° fiber tow cracks developed during the first stage followed by an accelerated growth rate and reduced 90° tow crack density at saturation. The integrated digital imaging technique proved to effectively correlate damage events with stiffness degradation, leading to a deeper understanding of the fatigue behavior of glass fiber/thermoplastic composites.</div></div>\",\"PeriodicalId\":281,\"journal\":{\"name\":\"Composite Structures\",\"volume\":\"371 \",\"pages\":\"Article 119513\"},\"PeriodicalIF\":7.1000,\"publicationDate\":\"2025-07-24\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Composite Structures\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0263822325006786\",\"RegionNum\":2,\"RegionCategory\":\"材料科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"MATERIALS SCIENCE, COMPOSITES\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Composite Structures","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0263822325006786","RegionNum":2,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"MATERIALS SCIENCE, COMPOSITES","Score":null,"Total":0}
Integrated digital imaging technique for correlation of damage evolution and stiffness degradation in non-crimp fabric composite materials under cyclic loading
A novel integrated digital imaging technique was developed to automatically characterize damage and simultaneously monitor stiffness degradation in non-crimp fabric glass fiber/reactive thermoplastic cross-ply laminates subject to tension–tension cyclic loading. Under a peak stress of 50 % UTS, the laminate exhibited four distinct stages of stiffness degradation, including a significant drop during the first cycle due to 90° fiber tow crack initiation, a gradual decrease due to crack multiplication and propagation up to saturation, a stable phase comprising localized delamination crack propagation, and a sudden drop prior to specimen failure. Under a peak stress of 75 % UTS, both 0° and 90° fiber tow cracks developed during the first stage followed by an accelerated growth rate and reduced 90° tow crack density at saturation. The integrated digital imaging technique proved to effectively correlate damage events with stiffness degradation, leading to a deeper understanding of the fatigue behavior of glass fiber/thermoplastic composites.
期刊介绍:
The past few decades have seen outstanding advances in the use of composite materials in structural applications. There can be little doubt that, within engineering circles, composites have revolutionised traditional design concepts and made possible an unparalleled range of new and exciting possibilities as viable materials for construction. Composite Structures, an International Journal, disseminates knowledge between users, manufacturers, designers and researchers involved in structures or structural components manufactured using composite materials.
The journal publishes papers which contribute to knowledge in the use of composite materials in engineering structures. Papers deal with design, research and development studies, experimental investigations, theoretical analysis and fabrication techniques relevant to the application of composites in load-bearing components for assemblies, ranging from individual components such as plates and shells to complete composite structures.