American Society for Composites 2018最新文献

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Progressive Damage and Failure Prediction of Interlaminar Tensile Specimen with Initial Fabrication Induced Defects 带有初始制造缺陷的层间拉伸试样的渐进损伤和失效预测
American Society for Composites 2018 Pub Date : 2018-11-07 DOI: 10.12783/ASC33/26089
Xiaodong Cui, A. Karuppiah, D. Pham, J. Lua, C. Saathoff, W. Seneviratne
{"title":"Progressive Damage and Failure Prediction of Interlaminar Tensile Specimen with Initial Fabrication Induced Defects","authors":"Xiaodong Cui, A. Karuppiah, D. Pham, J. Lua, C. Saathoff, W. Seneviratne","doi":"10.12783/ASC33/26089","DOIUrl":"https://doi.org/10.12783/ASC33/26089","url":null,"abstract":"","PeriodicalId":337735,"journal":{"name":"American Society for Composites 2018","volume":"16 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-11-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122139479","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 3
Microscale Analysis of Virtually Cured Polymer Matrix Composites Accounting for Uncertainty in Matrix Properties During Manufacturing 考虑制造过程中基体性能不确定性的虚拟固化聚合物基复合材料的微尺度分析
American Society for Composites 2018 Pub Date : 2018-11-07 DOI: 10.12783/ASC33/25958
Sagar P. Shah, M. Maiarù
{"title":"Microscale Analysis of Virtually Cured Polymer Matrix Composites Accounting for Uncertainty in Matrix Properties During Manufacturing","authors":"Sagar P. Shah, M. Maiarù","doi":"10.12783/ASC33/25958","DOIUrl":"https://doi.org/10.12783/ASC33/25958","url":null,"abstract":"This paper proposes a study on mechanical properties of virtually cured microstructures accounting for uncertainty in matrix properties and fiber packing. Computations are carried out using the finite element method (FEM) using the commercial code Abaqus supplemented by user written subroutines. An instantaneous linear elastic model for the stress evolution during manufacturing is employed to model curing. Results are presented in terms of transverse stiffness and strength for cured microstructures of different sizes. Comparisons are proposed with models not including curing induced residual stresses.","PeriodicalId":337735,"journal":{"name":"American Society for Composites 2018","volume":"215 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-11-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115977852","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 12
Effect of Manufacturing-Induced Voids on the Fatigue Performances of Multidirectional Laminates 制造诱导空洞对多向层压板疲劳性能的影响
American Society for Composites 2018 Pub Date : 2018-11-07 DOI: 10.12783/ASC33/25994
M. Quaresimin, L. Maragoni, P. Carraro
{"title":"Effect of Manufacturing-Induced Voids on the Fatigue Performances of Multidirectional Laminates","authors":"M. Quaresimin, L. Maragoni, P. Carraro","doi":"10.12783/ASC33/25994","DOIUrl":"https://doi.org/10.12783/ASC33/25994","url":null,"abstract":"In the present work, an overview is presented on the recent work carried out by the authors on the influence of manufacturing-induced porosity on the long-term performances of composite materials. The effect of voids was first studied in terms of fatigue damage mechanisms at the micro-scale. An extensive experimental campaign was then carried out to assess the effect of porosity on the life to crack initiation (S-N curves), crack propagation (Paris curve), crack density evolution and global stiffness drop of [0/902]S and [0/452/0/-452]S laminates. Finally, a model that allows to predict the life to crack initiation from the behaviour of the void-free material was developed, showing good accordance with the experimental results.","PeriodicalId":337735,"journal":{"name":"American Society for Composites 2018","volume":"157 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-11-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122450402","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Compressive Strength Prediction of 3D Woven Textile Composites: Single RVE Multiscale Analysis and Imperfection Sensitivity Study 三维纺织复合材料抗压强度预测:单RVE多尺度分析及缺陷敏感性研究
American Society for Composites 2018 Pub Date : 2018-11-07 DOI: 10.12783/ASC33/26103
D. Patel, A. Waas
{"title":"Compressive Strength Prediction of 3D Woven Textile Composites: Single RVE Multiscale Analysis and Imperfection Sensitivity Study","authors":"D. Patel, A. Waas","doi":"10.12783/ASC33/26103","DOIUrl":"https://doi.org/10.12783/ASC33/26103","url":null,"abstract":"","PeriodicalId":337735,"journal":{"name":"American Society for Composites 2018","volume":"256 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-11-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121244853","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Molecular Dynamics Simulations of Fiber-Sizing Interphase 纤维上浆间相的分子动力学模拟
American Society for Composites 2018 Pub Date : 2018-11-07 DOI: 10.12783/asc33/25917
S. Chowdhury, Ethan A. Wise, R. Elder, T. Sirk, D. Hartman, John Gillespie
{"title":"Molecular Dynamics Simulations of Fiber-Sizing Interphase","authors":"S. Chowdhury, Ethan A. Wise, R. Elder, T. Sirk, D. Hartman, John Gillespie","doi":"10.12783/asc33/25917","DOIUrl":"https://doi.org/10.12783/asc33/25917","url":null,"abstract":"","PeriodicalId":337735,"journal":{"name":"American Society for Composites 2018","volume":"7 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-11-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116467135","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
A Novel Test Method to Induce Bi-Axial Stress States in Thin-Ply Carbon Composites Under Combined Longitudinal Tension and Transverse Compression 在纵向拉伸和横向压缩联合作用下诱导薄层碳复合材料双轴应力状态的新型测试方法
American Society for Composites 2018 Pub Date : 2018-11-07 DOI: 10.12783/asc33/25937
Tamas Rev, G. Czél, M. Wisnom
{"title":"A Novel Test Method to Induce Bi-Axial Stress States in Thin-Ply Carbon Composites Under Combined Longitudinal Tension and Transverse Compression","authors":"Tamas Rev, G. Czél, M. Wisnom","doi":"10.12783/asc33/25937","DOIUrl":"https://doi.org/10.12783/asc33/25937","url":null,"abstract":"A novel test configuration has been developed to induce combined stress-states of inplane longitudinal tension and transverse compression in unidirectional (UD) composite layers. Two different multi-directional laminates have been designed incorporating UD carbon/epoxy plies embedded in angle-ply blocks of the same material. The scissoring deformation of the angle-plies induces compression in the central UD layers when the composite is strained in the 0° fibre direction. The amount of transverse compressive stress is determined through an inverse identification method from the measured surface strains of the laminates. Despite the large in-plane transverse compressive strain generated, there is only about 9% drop in the failure strain of the laminates when compared to the baseline failure strain of the UD carbon/epoxy material.","PeriodicalId":337735,"journal":{"name":"American Society for Composites 2018","volume":"44 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-11-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"126992011","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 3
A Continuum Damage Model for Fatigue and Its Integration Scheme 疲劳连续损伤模型及其积分方案
American Society for Composites 2018 Pub Date : 2018-11-07 DOI: 10.12783/ASC33/26169
Z. Gao, Liang Zhang, R. Haynes, Wenbin Yu
{"title":"A Continuum Damage Model for Fatigue and Its Integration Scheme","authors":"Z. Gao, Liang Zhang, R. Haynes, Wenbin Yu","doi":"10.12783/ASC33/26169","DOIUrl":"https://doi.org/10.12783/ASC33/26169","url":null,"abstract":"The objective of this paper is to develop a continuum damage model for fatigue prediction. A viscodamage model, which can rigorously handle damage anisotropy, distinct tensile and compressive damage behavior, and damage deactivation, is developed to produce stress-dependent fatigue damage evolution. An affine formulation governing damage evolution, and a closed-form formulation of the constitutive relations is derived based on the viscodamage model. An adaptive stepsize control and cycle jump time integration scheme is proposed and implemented to improve the present model’s efficiency in cyclic loading conditions. Through uniaxial cyclic loading simulations, the present model and time integration scheme is found to be capable of reliably and efficiently producing cyclic damage evolution. This model can be further calibrated to facilitate both uniaxial and multiaxial fatigue analysis in composite materials.","PeriodicalId":337735,"journal":{"name":"American Society for Composites 2018","volume":"37 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-11-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127068845","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Multiscale Modeling of the Impact Response of Triaxially Braided Polymer Matrix Composites, Including Effects of Adiabatic Heating 包括绝热加热影响的三轴编织聚合物基复合材料冲击响应的多尺度建模
American Society for Composites 2018 Pub Date : 2018-11-07 DOI: 10.12783/ASC33/25997
C. Sorini, A. Chattopadhyay, R. Goldberg
{"title":"Multiscale Modeling of the Impact Response of Triaxially Braided Polymer Matrix Composites, Including Effects of Adiabatic Heating","authors":"C. Sorini, A. Chattopadhyay, R. Goldberg","doi":"10.12783/ASC33/25997","DOIUrl":"https://doi.org/10.12783/ASC33/25997","url":null,"abstract":"Significant local temperature rises often accompany the high rate deformation of polymer matrix composites. In the case of impact loading, heat is generated locally within the polymer matrix due to plastic dissipation, but the rapid nature of the loading precludes significant heat transfer from occurring; ballistic impact loading can therefore be regarded as fully adiabatic. In this paper, the development of a synergistic multiscale approach to simulate the architecturally dependent impact response of polymer matrix composites with complex fiber tow architectures is presented and applied to a representative triaxially braided composite material system. To approximate the heterogeneity of the composite braid architecture at the highest analysis length scale, a subcell-based approach is utilized whereby the mesoscale repeating unit cell of the material is discretized in-plane into an assemblage of laminated composite subcell regions, with stacking sequences determined from the braid architecture. Each unidirectional layer of the laminated composite subcells are modeled with the generalized method of cells micromechanics theory, where a nonisothermal viscoplastic constitutive model is employed to model the rate, temperature, and pressure dependent polymer matrix. Matrix temperature rises due to inelastic deformation are computed. in matrix elastic properties are determined from neat resin dynamic mechanical analysis data. The commercial transient dynamic finite element code LS-DYNA is utilized to conduct simulations of quasi-static coupon tests and flat panel impact tests performed on a T700/PR520 [0°/60°/–60°] triaxially braided composite. Good agreement is found between simulations and experiments. It is expected that, once progressive damage and failure are incorporated into the multiscale scheme, the incorporation of adiabatic heating affects will greatly improve the predictive capability of current models.","PeriodicalId":337735,"journal":{"name":"American Society for Composites 2018","volume":"59 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-11-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127160399","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Reactive Molecular Dynamics Simulation of Accelerated Cross-linking and Disintegration of Bisphenol F/DETDA Polymer using ReaxFF 利用 ReaxFF 对双酚 F/DETDA 聚合物的加速交联和分解进行反应分子动力学模拟
American Society for Composites 2018 Pub Date : 2018-11-07 DOI: 10.12783/ASC33/25939
Aniruddh Vashisth, Chowdhury M. Ashraf, C. Bakis, A. Duin
{"title":"Reactive Molecular Dynamics Simulation of Accelerated Cross-linking and Disintegration of Bisphenol F/DETDA Polymer using ReaxFF","authors":"Aniruddh Vashisth, Chowdhury M. Ashraf, C. Bakis, A. Duin","doi":"10.12783/ASC33/25939","DOIUrl":"https://doi.org/10.12783/ASC33/25939","url":null,"abstract":"Molecular dynamics simulations of polymers can help in understanding the dependence of molecular structure, cross-linking and the chemistry of the polymer chain and resulting thermo-mechanical properties of the polymer. Apart from these thermo-mechanical properties, molecular dynamics is also a powerful tool to examine the durability of polymers with potential aerospace applications under harsh environmental conditions. Ultraviolent radiation from the sun results in dissociation of molecular oxygen into atomic oxygen (AO) which is abundant in lower earth orbit. Testing composites under AO impact requires an extensive experimental setup to simulate low earth orbit (LEO) conditions and is therefore expensive. Using a newly developed accelerated cross-linking methodology in the framework of ReaxFF, bisphenol F and diethyltoluenediamine epoxy polymer chains are manufactured virtually. This simulated polymer is virtually tested for modulus, glass transition temperature, density and is impacted by atomic oxygen at 8 km/s. Thermomechanical properties show good agreement between experiments and simulations. Simulations the polymer during AO impact using ReaxFF provides useful insight to the degradation mechanism in terms of polymer chemistry and thermal profile.","PeriodicalId":337735,"journal":{"name":"American Society for Composites 2018","volume":"97 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-11-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"127219191","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 4
Closed-Form Mixed-Mode Strain Energy Release Rate Expressions for Unidirectional Laminate Configurations 单向层压板结构的封闭形式混合模应变能释放率表达式
American Society for Composites 2018 Pub Date : 2018-11-07 DOI: 10.12783/ASC33/26094
Patrick Enjuto, G. Mabson
{"title":"Closed-Form Mixed-Mode Strain Energy Release Rate Expressions for Unidirectional Laminate Configurations","authors":"Patrick Enjuto, G. Mabson","doi":"10.12783/ASC33/26094","DOIUrl":"https://doi.org/10.12783/ASC33/26094","url":null,"abstract":"A closed-form fracture methodology based on first order shear deformable plate theory (FSDT) was developed in Reference [1]. By using a sub-laminate model and adopting transverse shear-deformable laminate theory, general expressions for total strain energy-release rate (SERR) and its individual components were derived. Making use of the first order shear deformable plate theory, closed-form expressions for the calculation of the individual modes of the strain energy release rate for traditional unidirectional laminate test specimens used to obtain fracture toughness properties (Double Cantilever Beam, End Notch Flexure and Mixed-Mode Bending) are presented.","PeriodicalId":337735,"journal":{"name":"American Society for Composites 2018","volume":"25 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2018-11-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"125661084","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 2
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