Low-velocity impact size effect of carbon fiber composite laminates: Experimental and mechanism research

IF 6.6 1区 工程技术 Q1 ENGINEERING, CIVIL
Songjing Liu , Yanwei Ding , Yu Feng , Wenqian Wang , Chunwang Niu , Jialu Wang
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Abstract

The low-velocity impact (LVI) response characteristics of carbon fiber composite laminates under the influence of the size effect was investigated. Firstly, LVI experiments were conducted on composite laminates with varying in-plane dimensions and thicknesses under different impact energies to analyze their LVI response patterns. Secondly, non-destructive testing methods were utilized to examine the surface and internal damage conditions of the laminates, elucidating the LVI damage response characteristics influenced by the size effect. Finally, high-speed imaging and scanning electron microscopy (SEM) techniques were employed in conjunction to reveal the underlying mechanisms of the size effect during LVI on composite laminates. The findings indicate that under identical impact energy conditions, as the in-plane dimension of the laminate increases (with constant thickness), the peak force and absorbed energy progressively decrease, while the maximum displacement increases. Additionally, the degree of surface damage diminishes, and the projected area of internal damage reduces and becomes more concentrated near the impact surface in the depth direction. As the thickness of the laminate increases (with constant in-plane dimension), the peak force and the slope K value of the Displacement-Time curve increase, whereas the absorbed energy initially decreases and then slightly rises, the maximum displacement decreases, the degree of surface damage weakens, and the projected area of internal damage expands. An increase in the in-plane dimension of the laminate facilitates the absorption and dissipation of impact energy through elastic deformation, thereby reducing the extent of internal damage. Meanwhile, an increase in laminate thickness enhances the likelihood of matrix damage and delamination damage propagation. The initiation and propagation of damage across multiple layers of the matrix absorb a significant portion of the impact energy, consequently mitigating fiber fracture damage.
碳纤维复合材料层合板低速冲击尺寸效应:实验与机理研究
研究了碳纤维复合材料层合板在尺寸效应影响下的低速冲击响应特性。首先,对不同面内尺寸和厚度的复合材料层合板在不同冲击能量下进行LVI实验,分析其LVI响应模式。其次,采用无损检测方法对层合板的表面和内部损伤情况进行了检测,阐明了尺寸效应对层合板LVI损伤响应特性的影响。最后,利用高速成像和扫描电子显微镜(SEM)技术,揭示了复合材料层合板LVI过程中尺寸效应的潜在机制。结果表明:在相同冲击能条件下,随着层合板面内尺寸的增大(厚度不变),峰值力和吸收能逐渐减小,最大位移增大;表面损伤程度减小,内部损伤投影面积减小,且在深度方向上更集中于撞击面附近。随着层合板厚度的增加(面内尺寸不变),峰值力和位移-时间曲线斜率K值增大,而吸收能量先减小后略有上升,最大位移减小,表面损伤程度减弱,内部损伤投影面积扩大。增加层合板的面内尺寸有利于通过弹性变形吸收和消散冲击能,从而减小内部损伤程度。同时,层合层厚度的增加增加了基体损伤和分层损伤扩展的可能性。损伤在多层基体上的发生和扩展吸收了很大一部分冲击能量,从而减轻了纤维断裂损伤。
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来源期刊
Thin-Walled Structures
Thin-Walled Structures 工程技术-工程:土木
CiteScore
9.60
自引率
20.30%
发文量
801
审稿时长
66 days
期刊介绍: Thin-walled structures comprises an important and growing proportion of engineering construction with areas of application becoming increasingly diverse, ranging from aircraft, bridges, ships and oil rigs to storage vessels, industrial buildings and warehouses. Many factors, including cost and weight economy, new materials and processes and the growth of powerful methods of analysis have contributed to this growth, and led to the need for a journal which concentrates specifically on structures in which problems arise due to the thinness of the walls. This field includes cold– formed sections, plate and shell structures, reinforced plastics structures and aluminium structures, and is of importance in many branches of engineering. The primary criterion for consideration of papers in Thin–Walled Structures is that they must be concerned with thin–walled structures or the basic problems inherent in thin–walled structures. Provided this criterion is satisfied no restriction is placed on the type of construction, material or field of application. Papers on theory, experiment, design, etc., are published and it is expected that many papers will contain aspects of all three.
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