Show simple item record

dc.contributor.advisorRaúl Radovitzky.en_US
dc.contributor.authorWalcher, Bradley James,Jr.en_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2019-10-04T21:33:29Z
dc.date.available2019-10-04T21:33:29Z
dc.date.copyright2019en_US
dc.date.issued2019en_US
dc.identifier.urihttps://hdl.handle.net/1721.1/122418
dc.descriptionThesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2019en_US
dc.descriptionCataloged from PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (pages 73-75).en_US
dc.description.abstractIt has long been known current helmet test methodology suffers from a missing connection between helmet test standards and the relevance to injury prevention. One of the tests in the protocol consists of impacting the helmet material plates with a high-velocity projectile and the performance assessment is based on the permanent deformation of the backing-material, Roma Plastilina clay. This work focuses on the development of a computational framework to develop a deeper understanding of the mechanical response of Roma Plastilina clay. Prior work has focused on the development of a clay model based on Cam-clay theory. In this work, it is shown this model failed to adequately capture the mechanical response across the range of strain rates of interest. To address this deficiency, the previous model formulation is extended to a more general rate-dependence model of the power-law type. Three impact tests are used to calibrate the modified constitutive model for the clay: one low-velocity test and two high-velocity tests. The low-velocity test is a drop test used to ensure the clay is well-conditioned for the high-velocity tests in which a high-velocity projectile impacts a plate with a clay backing. The final clay deformation for all three tests is compared against experimental data to ensure the accuracy of the clay model. Finally, to improve simulation efficiency, scalability of the computational framework is tested. It is concluded the computational framework is an effective tool for modeling Roma Plastilina clay. The constitutive model for the Roma Plastilina clay is validated, tested and final material parameters are determined that characterize the clay behavior over a large range of impact rates. The modified clay model is used to explore the phenomenon of separation between the plate and clay which was previously believed to only occur with hard plate materials.en_US
dc.description.statementofresponsibilityby Bradley James Walcher Jr.en_US
dc.format.extent83 pagesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsMIT theses are protected by copyright. They may be viewed, downloaded, or printed from this source but further reproduction or distribution in any format is prohibited without written permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleComputational modeling of the impact response of Roma Plastilina across a wide range of strain ratesen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.identifier.oclc1120047868en_US
dc.description.collectionS.M. Massachusetts Institute of Technology, Department of Aeronautics and Astronauticsen_US
dspace.imported2019-10-04T21:33:27Zen_US
mit.thesis.degreeMasteren_US
mit.thesis.departmentAeroen_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record