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dc.contributor.advisorAdnan, Ashfaq
dc.creatorQasaimeh, Momen Mohammad
dc.date.accessioned2022-08-24T17:32:25Z
dc.date.available2022-08-24T17:32:25Z
dc.date.created2021-08
dc.date.issued2021-08-16
dc.date.submittedAugust 2021
dc.identifier.urihttp://hdl.handle.net/10106/30908
dc.description.abstractFused filament fabrication (FFF) is one of the most common additive manufacturing/3D printing techniques where continuously extruded semi-molten filaments are deposited in a layer-by-layer manner. The quality of the manufactured part depends on some major factors such as filament-filament contact and adhesion as well as the void fraction. Filament to filament adhesion affects the part strength under transverse load. In our earlier work, we studied the effect of in situ ball rolling on the thermal and mechanical properties of the printed parts. It was found that when printing/rolling parameters are correctly tuned and in situ compression rolling is appropriately applied over the depositing filaments, a significant increase in material toughness and tensile strength are realized. Here, we have developed an integrated model that includes the in situ compression rolling and filament-filament contact during deposition. The rolling parameters such as ball weight, ball temperature, filament temperature are explicitly included in the model. The effect of these parameters on the part height, void fraction, and filament adhesion are studied. Based on JKR contact theory and the theory of elasticity, our mathematical model predicts the evolution of filament-to-filament contact width and corresponding void fraction and part height in the representative volume element of the simulated printed part. Our prediction matches fairly well with the previous experimental results. We have also optimized the filament temperature during the rolling process. We find that the maximum adhesion between filaments occurs when the two filaments are brought close to isothermal contact. We have concluded that parts fabricated from a system integrated with an in-situ preheating and in situ post-rolling would yield the most effective part. The next step to fulfill this research's scope is to study the fracture behavior of printed filaments in contact. We have considered the effect of the contact half-width and the impact of the shape of the filament cross-section (filaments mesostructured) on the fracture strength and on mode  stress intensity factor (SIF) at the crack tip. The results show that the rolled filaments have a longer contact half-width and larger notch angle at the interface between the filaments, which means higher singularity order and better fracture properties. A 3 point bending test has been conducted to measure the fracture strength for rolled and baseline v-notch samples. The rolled part’s strength shows double the baseline part strength. A computational study has been formed to predict fracture behavior. We found that at longer filament-filament contact width, the part has a higher critical stress intensity factor and slower crack propagation. We believe that studying the fracture behavior of the printed filaments under different temperatures will add significant knowledge to industrial applications like 3d printed electronic devices or 3d printed heat exchangers. So, we have tested the rolled part’s strength at different temperatures. As expected, the temperature increase results in less fracture strength and more ductile behavior.
dc.format.mimetypeapplication/pdf
dc.language.isoen_US
dc.subject3D printing
dc.subjectFracture mechanics
dc.subjectAdditive manufacturing
dc.subjectPLA thermoplastic
dc.subjectVoid reduction
dc.subjectMechanical behavior
dc.subjectDeformation
dc.titleMODELING THE EFFECT OF IN SITU NOZZLE-INTEGRATED COMPRESSION ROLLING ON THE MECHANICAL AND FRACTURE BEHAVIOR OF FUSED FILAMENT FABRICATION (FFF) 3D PRINTED PARTS
dc.typeThesis
dc.degree.departmentMechanical and Aerospace Engineering
dc.degree.nameDoctor of Philosophy in Mechanical Engineering
dc.date.updated2022-08-24T17:32:25Z
thesis.degree.departmentMechanical and Aerospace Engineering
thesis.degree.grantorThe University of Texas at Arlington
thesis.degree.levelDoctoral
thesis.degree.nameDoctor of Philosophy in Mechanical Engineering
dc.type.materialtext
dc.creator.orcid0000-0002-1913-1612


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