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dc.contributor.advisorGururaja, Suhasini
dc.contributor.authorShashidhar, K
dc.date.accessioned2026-02-27T05:05:22Z
dc.date.available2026-02-27T05:05:22Z
dc.date.submitted2026
dc.identifier.urihttps://etd.iisc.ac.in/handle/2005/8752
dc.description.abstractThe current work examines how process-induced defects influence the compressive behavior of composite structures. The defects analyzed include wrinkles at the macroscale and fiber misalignment at the microscale. Uni-directional carbon fiber reinforced polymer composites with intentionally created wrinkles were produced by strategically positioning laminate strips. Through comprehensive experimental characterization, the research thoroughly investigates the impact of wrinkle characteristics and their locations on compressive strength and failure modes. Furthermore, the study explores how these wrinkle features affect the final kink bandwidth, angle, and inclination. Fractographic analysis of the failed specimens identified several damage modes across different length scales, such as kinking, delamination, buckle delamination, crushing, fiber pullout, matrix cracking or failure, and fiber failure. These findings highlight the importance of considering the geometry of the wrinkles and the various damage modes at different scales when creating a numerical model to accurately predict the compressive behavior of the composite. Utilizing the damage modes identified through experimentation, a three dimensional repeating unit cell framework is used to investigate how various competing damage mechanisms-such as fiber failure, matrix plasticity and cracking, and fiber/matrix debonding-impact the compressive behavior of the composite material. A series of parametric studies is performed to evaluate the effects of factors like fiber volume fraction, fiber misalignment, and interfacial properties (including strength, fracture energies, and friction) on compressive performance. The results reveal a strong correlation between compressive strength and kink band characteristics with fiber volume fraction, fiber misalignment, interfacial shear strength, interfacial friction, and matrix cracking. This highlights the necessity of accurately characterizing the mechanical properties and geometric features of the composite constituents. To account for the impact of realistic microstructures on compressive behavior, a two-step homogenization process has been proposed to reduce computational demands and improve the efficiency of the numerical model. In the first step, the model captures the homogenized elastic properties and longitudinal compressive behavior. These properties are then used as inputs for a model that consists of multiple domains discretized with Voronoi polygons, each assigned a specific initial fiber misalignment angle based on a statistical distribution. The homogenized compressive behavior has been validated against previous studies and shows strong agreement. Additionally, the proposed method has the potential to develop into a multiscale modeling strategy that predicts compressive behavior by considering variations in realistic microstructural characteristicsen_US
dc.language.isoen_USen_US
dc.relation.ispartofseries;ET01280
dc.rightsI grant Indian Institute of Science the right to archive and to make available my thesis or dissertation in whole or in part in all forms of media, now hereafter known. I retain all proprietary rights, such as patent rights. I also retain the right to use in future works (such as articles or books) all or part of this thesis or dissertationen_US
dc.subjectcomposite structuresen_US
dc.subjectcompositesen_US
dc.subjectDefectsen_US
dc.subjectcarbon fiber reinforced polymer compositeen_US
dc.subjectWrinklesen_US
dc.subjectCrackingen_US
dc.subject.classificationResearch Subject Categories::TECHNOLOGY::Engineering mechanicsen_US
dc.titleCompressive behavior of continuous fiber polymer composites in the presence of process-induced defectsen_US
dc.typeThesisen_US
dc.degree.namePhDen_US
dc.degree.levelDoctoralen_US
dc.degree.grantorIndian Institute of Scienceen_US
dc.degree.disciplineEngineeringen_US


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