VTechWorks staff will be away for the Thanksgiving holiday beginning at noon on Wednesday, November 27, through Friday, November 29. We will resume normal operations on Monday, December 2. Thank you for your patience.
 

Geometric and material nonlinear analysis of laminated composite plates and shells

dc.contributor.authorChandrashekhara, K.en
dc.contributor.committeechairReddy, Junuthula N.en
dc.contributor.committeememberFrederick, Danielen
dc.contributor.committeememberSmith, C.W.en
dc.contributor.committeememberHenneke, Edmund G.en
dc.contributor.committeememberPlaut, Raymond H.en
dc.contributor.departmentEngineering Mechanicsen
dc.date.accessioned2015-07-28T19:21:11Zen
dc.date.available2015-07-28T19:21:11Zen
dc.date.issued1985en
dc.description.abstractAn inelastic material model for laminated composite plates and shells is formulated and incorporated into a finite element model that accounts for both geometric nonlinearity and transverse shear stresses. The elasto-plastic material behavior is incorporated using the flow theory of plasticity. In particular, the modified version of Hill's initial yield criterion is used in which anisotropic parameters of plasticity are introduced with isotropic strain hardening. The shear deformation is accounted for using an extension of the Sanders shell theory and the geometric nonlinearity is considered in the sense of the von Karman strains. A doubly curved isoparametric rectangular element is used to model the shell equations. The layered element approach is adopted for the treatment of plastic behavior through the thickness. A wide range of numerical examples is presented for both static and dynamic analysis to demonstrate the validity and efficiency of the present approach. The results for combined nonlinearity are also presented. The results for isotropic results are in good agreement with those available in the literature. The variety of results presented here based on realistic material properties of more commonly used advanced laminated composite plates and shells should serve as references for future investigations.en
dc.description.degreePh. D.en
dc.format.extentiv, 114 leavesen
dc.format.mimetypeapplication/pdfen
dc.identifier.urihttp://hdl.handle.net/10919/54739en
dc.language.isoen_USen
dc.publisherVirginia Polytechnic Institute and State Universityen
dc.relation.isformatofOCLC# 14094654en
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subject.lccLD5655.V856 1985.C525en
dc.subject.lcshLaminated materials -- Analysisen
dc.subject.lcshShells (Engineering) -- Plastic propertiesen
dc.subject.lcshPlates (Engineering) -- Plastic propertiesen
dc.subject.lcshStructural analysis (Engineering) -- Mathematical modelsen
dc.subject.lcshFinite element methoden
dc.titleGeometric and material nonlinear analysis of laminated composite plates and shellsen
dc.typeDissertationen
dc.type.dcmitypeTexten
thesis.degree.disciplineEngineering Mechanicsen
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen
thesis.degree.leveldoctoralen
thesis.degree.namePh. D.en

Files

Original bundle
Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
LD5655.V856_1985.C525.pdf
Size:
2.56 MB
Format:
Adobe Portable Document Format