Peridynamic Investigation of Stress-Strain Response and Fracture Behavior Variations in Micro-CT Images of Mock Energetic Nanocomposites

dc.contributor.authorSpinetta, Anthony Kumaren
dc.contributor.committeechairSeidel, Gary D.en
dc.contributor.committeememberKapania, Rakesh K.en
dc.contributor.committeememberPhilen, Michael Keithen
dc.contributor.departmentAerospace and Ocean Engineeringen
dc.date.accessioned2025-06-07T08:04:48Zen
dc.date.available2025-06-07T08:04:48Zen
dc.date.issued2025-06-06en
dc.description.abstractThe stress-strain response and fracture behaviors of a mock energetic nanocomposite were investigated to reveal behaviors that contribute to variations throughout the sample. Approximately 100 XCT images that span the depth of a single sample were modeled in a peridynamics formulation to investigate changes in behaviors throughout the composite. The meshes, which included sugar, PDMS, and void phases, were modeled using tensile boundary conditions. The results from the y-direction elastic cases suggest that the overall sample had an effective stiffness of 4.396 +/- 1.153 GPa, though this varied significantly between images and image groupings. In addition, the effective stiffness of image groupings varied from 2.5 GPa to approximately 5 GPa as image number increased. These computationally determined effective stiffnesses were compared to the Mori-Tanaka approach for effective material property estimation, and the results were broadly consistent with the Mori-Tanaka solution. Damage-enabled cases were also conducted, and the results from the y-direction cases revealed unique characteristics associated with damage propagation for specific images. While the majority of the stress vs. strain curves displayed gradual damage evolution, some images exhibited rapid damage evolution caused by loading columns due to tightly packed sugar grains. In addition, variations were also caused by connection points, bridging the two halves of the mesh across voids. The variation of ultimate stress with respect to image number was also investigated, suggesting a slight increase in ultimate stress with image number. The combination of elastic and damage-enabled results displayed a general increase in stiffness for the material as image number increased. The isotropy investigation and averaged results indicated that the composite was transversely isotropic. The stress vs. strain curve for the damage-enabled cases were nearly identical for the y-direction and x-direction conditions, with a maximum percent difference of 16.4% for the duration of the simulation. The transverse isotropy was especially evident in the elastic comparison, where the average stress values had a maximum percent difference of 1.3% between strain values of 0.03% and 1%. The simulations also indicated an increase in effective stiffness and peak stress as a function of image number. Overall, the results demonstrate that the sample is statistically heterogeneous for both effective stiffness and fracture behavior. In addition, variations in effective material properties with respect to image number suggest the necessity to include this variability in sampling and modeling strategies. The fracture behaviors were also highly sensitive to the microstructure configurations, and would therefore need to be accounted for when characterizing this composite in advanced piezoresistive models.en
dc.description.abstractgeneralThe stress-strain response and damage behaviors of an energetic composite were investigated to reveal behaviors that contribute to variations throughout the sample. Approximately 100 x-ray images of a single sample were modeled in a continuum mechanics formulation, peridynamics, to investigate changes in behaviors across the images, or depth, of the sample. The meshes, which included sugar and PDMS materials, were modeled in a mechanical formulation. The results from the y-direction, no-damage cases suggest that the overall sample had an effective stiffness of 4.396 +/- 1.153 GPa, though this varied significantly between images and image groupings. In addition, the effective stiffness of image groupings varied from 2.5 GPa to approximately 5 GPa as image number increased. These computationally determined effective stiffnesses were compared to the Mori-Tanaka approach for effective material property estimation, and the results were broadly consistent with this analytical solution. The results from the y-direction, damage-enabled cases revealed unique characteristics associated with damage propagation for specific images. While the majority of images displayed gradual damage evolution, some images exhibited rapid damage evolution caused by high-stress columns due to tightly packed sugar grains. In addition, variations were also caused by connection points, bridging the two halves of the mesh across voids. The variation of peak stress with respect to image number was also investigated, suggesting a slight increase in ultimate stress with image number. The combination of no-damage and damage-enabled results displayed a general increase in stiffness for the material as image number increased. The investigation also included simulating the images in the x-direction, and this indicated that the average material response was symmetric. The stress vs. strain curve for the damage-enabled cases were nearly identical for the x-direction and y-direction conditions, with a maximum percent difference of 16.4% for the duration of the simulation. The no-damage comparison illustrated that the average stress values had a maximum percent difference of 1.3% between strain values of 0.03% and 1%. The simulations also indicated an increase in effective stiffness and peak stress as a function of image number. Overall, the results demonstrate that the sample has high variability across images and is not suitably represented by a single image. In addition, variations in effective material stiffness with respect to image number suggest the necessity to include this variability in sampling and modeling strategies.en
dc.description.degreeMaster of Scienceen
dc.format.mediumETDen
dc.identifier.othervt_gsexam:43825en
dc.identifier.urihttps://hdl.handle.net/10919/135412en
dc.language.isoenen
dc.publisherVirginia Techen
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subjectMultifunctional Nanocompositesen
dc.subjectEnergeticsen
dc.subjectPeridynamicsen
dc.subjectFracture Behaviorsen
dc.subjectSugar-PDMS Samplesen
dc.titlePeridynamic Investigation of Stress-Strain Response and Fracture Behavior Variations in Micro-CT Images of Mock Energetic Nanocompositesen
dc.typeThesisen
thesis.degree.disciplineAerospace Engineeringen
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen
thesis.degree.levelmastersen
thesis.degree.nameMaster of Scienceen

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