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dc.contributor.advisorKeshavanarayana, Suresh R.
dc.contributor.authorIvanov, Dmitrii
dc.date.accessioned2020-07-16T16:42:10Z
dc.date.available2020-07-16T16:42:10Z
dc.date.issued2020-05
dc.identifier.othert20015
dc.identifier.urihttps://soar.wichita.edu/handle/10057/18839
dc.descriptionThesis (M.S.)-- Wichita State University, College of Engineering, Dept. of Aerospace Engineering
dc.description.abstractThis research attempted to describe the geometry of HexWeb CR-III-1/8-5052-8.1N commercial aluminum honeycomb core and give some statistical information about its deviation from the average. The finite element model of hexagonal honeycomb aluminum core was developed and validated using uniaxial tension-compression experimental data. The model was used for studying the effect of the geometrical irregularities, residual stresses, and strains on in-plane mechanical behavior of material. The homogenized yielding envelope was obtained based on developed model. The node bond failure was observed to occur in a stable manner and contributed significantly to the overall yielding of the core when the loads were dominated by transverse tension.
dc.format.extentxiv, 130 pages
dc.language.isoen_US
dc.publisherWichita State University
dc.rightsCopyright 2020 by Dmitrii Ivanov All Rights Reserved
dc.subject.lcshElectronic dissertations
dc.titleDevelopment of homogenized elasto-plastic material behavior of hexagonal cell honeycomb core using experiments and finite element analysis
dc.typeThesis


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  • AE Theses and Dissertations
    Electronic copies of theses and dissertations defended in the Department of Aerospace Engineering
  • CE Theses and Dissertations
    Doctoral and Master's theses authored by the College of Engineering graduate students
  • Master's Theses
    This collection includes Master's theses completed at the Wichita State University Graduate School (Fall 2005 --)

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