Show simple item record

dc.contributor.advisorLagoudas, Dimitris
dc.contributor.advisorHartl, Darren
dc.creatorMartin, Daniel Thomas
dc.date.accessioned2020-08-26T19:00:14Z
dc.date.available2020-08-26T19:00:14Z
dc.date.created2019-12
dc.date.issued2019-09-17
dc.date.submittedDecember 2019
dc.identifier.urihttps://hdl.handle.net/1969.1/188774
dc.description.abstractShape Memory Alloys (SMAs) are a unique class of intermetallic alloys that can cyclically sustain large deformations and recover a designed geometry through a solid-to-solid, martensitic phase transformation. The multifunctional behavior of SMAs, being both structural and active, along with a favorable actuation energy density, make SMA actuators practical for volume, mass, and mechanical improvements to a system. For aerospace engineering applications, High Temperature SMAs (HTSMAs) are specialized to operate in the extreme environmental conditions necessary for safe operation in a higher temperature range. The main limitations to HTSMAs, however, are the unpredictable cyclic response and stability, large scale manufacturing inconsistency, and lack of commercially available design tools to accurately capture the macroscopic response. This study will address these limitations by characterizing cyclic evolution, using a single extrusion of high temperature SMA material for manufacturing and property consistency, and by developing and validating a finite element model to predict cyclic actuation response in bending loading conditions typical in SMA actuator components. Results show experiments for Ni50.3TiHf20 High Temperature SMA (HTSMA) including: differential scanning calorimetry, thermomechanical actuation cycling in tension and compression, thermomechanical actuation cycling under pure bending, and C-Ring bending. Since there is significant tension - compression asymmetry in SMA phase transformation, a full-field strain response is quantified for bending cases using Digital Image Correlation (DIC). The four point bending results contain a neutral axis shift due to the asymmetry, and during actuation cycling, the neutral axis continues to shift as a consequence of remnant, unrecovered plastic strains. C-ring tests show the martensitic phase transformation initiate in tension followed by compression during forward phase transformation. Lastly, two phenomenological, macroscopic SMA constitutive models that address cyclic behavior and anisotropy in SMA actuation are addressed. The constitutive models are used in a finite element software, Abaqus, with a user-defined material subroutine (UMAT) to address model improvements in light of the experimental results. Needed updates to the UMAT are discussed that will improve accuracy and prediction of the SMA actuation response in bending.en
dc.format.mimetypeapplication/pdf
dc.language.isoen
dc.subjectSMAsen
dc.subjectHTSMAsen
dc.subjectThermomechanical Actuation Cyclingen
dc.subjectTensionen
dc.subjectCompressionen
dc.subjectBendingen
dc.subjectSMA Constitutive Modelen
dc.titleExperimentation and Model Development of High Temperature Shape Memory Alloy Actuation Cycling Under Tension, Compression, and Bendingen
dc.typeThesisen
thesis.degree.departmentAerospace Engineeringen
thesis.degree.disciplineAerospace Engineeringen
thesis.degree.grantorTexas A&M Universityen
thesis.degree.nameMaster of Scienceen
thesis.degree.levelMastersen
dc.contributor.committeeMemberKaraman, Ibrahim
dc.type.materialtexten
dc.date.updated2020-08-26T19:00:15Z
local.etdauthor.orcid0000-0003-3903-2707


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record