James Finlay, A. Waas, P. Davidson, Jonathan D. Bartley-Cho, Nav Muraliraj
{"title":"Experimentally Validated Progressive Failure Modeling of Composite Pi Joints","authors":"James Finlay, A. Waas, P. Davidson, Jonathan D. Bartley-Cho, Nav Muraliraj","doi":"10.2514/1.j062625","DOIUrl":null,"url":null,"abstract":"A computational model has been developed to analyze composite pi joints subjected to pulloff and side-bend loading. A discrete damage modeling approach is used to capture the interactions between intralaminar damage (matrix cracking) and interlaminar damage (delamination). Cohesive element interlayers and matrix-crack elements are governed by the same mixed-mode traction–separation formulation, resulting in a unified damage framework. The finite element model was calibrated using experimental data from pristine and defective joints. In the calibration process, in situ cohesive material properties were backcalculated from pulloff tests such that the accurate prediction of structural response and the damage evolution of pi joints were possible. Computational predictions for both pulloff and side-bend loading are shown to agree well with experimental results for joints subjected to pulloff and side-bend loading.","PeriodicalId":7722,"journal":{"name":"AIAA Journal","volume":" ","pages":""},"PeriodicalIF":2.1000,"publicationDate":"2023-09-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"AIAA Journal","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.2514/1.j062625","RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0
Abstract
A computational model has been developed to analyze composite pi joints subjected to pulloff and side-bend loading. A discrete damage modeling approach is used to capture the interactions between intralaminar damage (matrix cracking) and interlaminar damage (delamination). Cohesive element interlayers and matrix-crack elements are governed by the same mixed-mode traction–separation formulation, resulting in a unified damage framework. The finite element model was calibrated using experimental data from pristine and defective joints. In the calibration process, in situ cohesive material properties were backcalculated from pulloff tests such that the accurate prediction of structural response and the damage evolution of pi joints were possible. Computational predictions for both pulloff and side-bend loading are shown to agree well with experimental results for joints subjected to pulloff and side-bend loading.
期刊介绍:
This Journal is devoted to the advancement of the science and technology of astronautics and aeronautics through the dissemination of original archival research papers disclosing new theoretical developments and/or experimental results. The topics include aeroacoustics, aerodynamics, combustion, fundamentals of propulsion, fluid mechanics and reacting flows, fundamental aspects of the aerospace environment, hydrodynamics, lasers and associated phenomena, plasmas, research instrumentation and facilities, structural mechanics and materials, optimization, and thermomechanics and thermochemistry. Papers also are sought which review in an intensive manner the results of recent research developments on any of the topics listed above.