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dc.contributor.advisorStricklin, James A.
dc.creatorWilke, Robert Arthur
dc.date.accessioned2020-08-21T21:01:31Z
dc.date.available2020-08-21T21:01:31Z
dc.date.issued1975
dc.identifier.urihttps://hdl.handle.net/1969.1/DISSERTATIONS-184810
dc.description.abstractA solution procedure is developed and evaluated for the solution of nonlinear dynamic structural problems. The nonlinear equations of motion are written using the finite element method with geometric nonlinearities and moderate rotations. The natural frequencies and mode shapes of the free vibration form of the equations are calculated and the mode shapes used to transform the equations of motion to another orthogonal coordinate system. In the transformed form the equations are uncoupled and may be integrated directly. This solution yields the displacements in the transformed coordinate system; these displacements are returned to the physical basis and used to evaluate the nonlinear terms for the next time. The process is repeated over the desired time range. The solution method is applied first to a simple geometrically nonlinear beam problem and then to a shell of revolution that has highly nonlinear response to the point load at its apex. The numerical results are evaluated for cases utilizing several numbers of mode shapes and are compared to a known convergent solution method. The conclusion reached is that economies in solution time and storage requirements can be effected by using a fraction of the full set of mode shapes and a larger time step than was hitherto permissible. The use of the solution method with existing computer codes and the convergence aspects of the method are discussed.en
dc.format.extent143 leavesen
dc.format.mediumelectronicen
dc.format.mimetypeapplication/pdf
dc.language.isoeng
dc.rightsThis thesis was part of a retrospective digitization project authorized by the Texas A&M University Libraries. Copyright remains vested with the author(s). It is the user's responsibility to secure permission from the copyright holder(s) for re-use of the work beyond the provision of Fair Use.en
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/
dc.subjectAerospace Engineeringen
dc.titleA finite element method for nonlinear dynamic analysis using a modal transformation matrixen
dc.typeThesisen
thesis.degree.disciplineAerospace Engineeringen
thesis.degree.grantorTexas A&M Universityen
thesis.degree.nameDoctor of Philosophyen
thesis.degree.namePh. D. in Aerospace Engineeringen
thesis.degree.levelDoctorialen
dc.contributor.committeeMemberHaisler, W. E.
dc.contributor.committeeMemberMartinez, J. E.
dc.contributor.committeeMemberPerry, W. L.
dc.type.genredissertationsen
dc.type.materialtexten
dc.format.digitalOriginreformatted digitalen
dc.publisher.digitalTexas A&M University. Libraries
dc.identifier.oclc5782563


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