Distributed optical sensing in composite laminates

Author:

Meadows Leeanna12,Sullivan Rani W1,Brown Kevin3,Ranatunga Vipul3,Vehorn Keith4,Olson Steven4

Affiliation:

1. Department of Aerospace Engineering, Mississippi State University, Mississippi State, MS, USA

2. Dynetics, Inc., Huntsville, AL, USA

3. Air Force Research Laboratory, Wright-Patterson AFB, Dayton, OH, USA

4. University of Dayton Research Institute, Dayton, OH, USA

Abstract

An optical fiber–based full-field strain measurement technique was used to investigate delamination growth in laminated composites. An experimental setup to load the test samples under idealized modes of delamination was used to investigate the ability to capture the shape and location of the delamination front. It is envisioned that the demonstrated approach has significant field applications in controlled laboratory settings where delaminations have to be located accurately. Furthermore, the ability of this measurement system to provide full-field strain measurements at any given pre-implanted location through the thickness overcomes the surface strain measurements obtained by digital image correlation. In order to demonstrate the technique, distributed fiber optic sensing is used to monitor the propagation of delaminations under pure mode I and II loading. Optical fibers were embedded one ply from the crack plane of both double cantilever beam and end notch flexure specimens. To establish a repeatable fabrication methodology, manufacturing techniques for embedding the optical fibers during the laminate layup process were established. Specimens with and without embedded fibers were tested to verify the fibers did not affect measured fracture toughness values. Crack lengths measured with the optical fibers compared well with true crack lengths, and measured strain distributions compared well with results from finite element analysis.

Publisher

SAGE Publications

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials,Modelling and Simulation

Cited by 14 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Influence of Stitch Angle on the Flexural Response of Composite Structures;Journal of Aircraft;2024-04-25

2. Estimating crack tip position in adhesively bonded joints subjected to mode II quasi‐static loading;Fatigue & Fracture of Engineering Materials & Structures;2024-01-24

3. Distributed strain sensing textile using a rosette pattern fiber sensor;Nondestructive Characterization and Monitoring of Advanced Materials, Aerospace, Civil Infrastructure, and Transportation XVII;2023-04-18

4. High-density Optical Fiber Sensing Network for Tri-axial Strain with Temperature Compensation;28th International Conference on Optical Fiber Sensors;2023

5. Strain-based delamination prediction in fatigue loaded CFRP coupon specimens by deep learning and static loading data;Composites Part B: Engineering;2022-07

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3