Date of Award
Fall 1992
Document Type
Thesis
Degree Name
Master of Science (MS)
Department
Mechanical & Aerospace Engineering
Program/Concentration
Engineering Mechanics
Committee Director
Nahil A. Sobh
Committee Member
Damodar R. Ambur
Committee Member
Stephen G. Cupschalk
Call Number for Print
Special Collections; LD4331.E57J38
Abstract
Continuous filament grid-stiffened structure is a stiffening concept that combines structural efficiency and damage tolerance. However, buckle resistant design of such structures using finite elements methods is expensive and time consuming. An analytical model of a general grid stiffened structure is developed using a smeared theory with a first order shear deformation theory to account for transverse shear flexibilities. The solution for buckling of a simply supported panel subjected to combined loading is developed using energy method and a Rayleigh-Ritz technique. The smeared theory results are compared with finite element results. The results smeared theory compare well with the finite element results.
Rights
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DOI
10.25777/jjr4-n357
Recommended Citation
Jaunky, Navin R..
"Elastic Buckling of Stiffened Composite Curved Panels"
(1992). Master of Science (MS), Thesis, Mechanical & Aerospace Engineering, Old Dominion University, DOI: 10.25777/jjr4-n357
https://digitalcommons.odu.edu/mae_etds/542