TY - GEN
T1 - Finite element approach to the static, vibration and buckling analysisof curvilinearly stiffened plates
AU - Shi, Peng
AU - Kapania, Rakesh K.
AU - Dong, C. Y.
N1 - Publisher Copyright:
© 2015, American Institute of Aeronautics and Astronautics Inc. All rights Reserved.
PY - 2015
Y1 - 2015
N2 - A finite element method based approach is developed for studying the static, vibration and buckling behavior of curvilinearly stiffened plates in the presence of in-plane compressive and tensile stresses. The first order shear deformation theory (FSDT) is employed for both the plate and the Timoshenko beam modeling. Interpolation functions are used to build the displacement mapping between the stiffener and the plate nodes to allow the stiffener to be placed anywhere within the plate. One of the advantages of the present method is that the plate need not be re-meshed while the stiffener configuration is changed, and second, results obtained by the present method with much fewer number of elements match well with the results obtained by using a commercial FEM software. Several numerical examples are solved to study both the static and dynamic behaviors of stiffened plates. The effects of boundary conditions, stiffener eccentricity, stiffener curvature, stiffener-plate geometry parameters, in-plane load condition, stiffener-plate cross-section area ratio and stiffness ratio on the static and dynamic behaviors of curvilinearly stiffened plate are investigated. Results have shown that behavior of the natural frequency parameter as a function of applied in-plane stress could be affected by the plate thickness, in-plane load condition, stiffener-plate cross-section area ratio and stiffness ratio during compression only, but not when subjected to in-plane tension.
AB - A finite element method based approach is developed for studying the static, vibration and buckling behavior of curvilinearly stiffened plates in the presence of in-plane compressive and tensile stresses. The first order shear deformation theory (FSDT) is employed for both the plate and the Timoshenko beam modeling. Interpolation functions are used to build the displacement mapping between the stiffener and the plate nodes to allow the stiffener to be placed anywhere within the plate. One of the advantages of the present method is that the plate need not be re-meshed while the stiffener configuration is changed, and second, results obtained by the present method with much fewer number of elements match well with the results obtained by using a commercial FEM software. Several numerical examples are solved to study both the static and dynamic behaviors of stiffened plates. The effects of boundary conditions, stiffener eccentricity, stiffener curvature, stiffener-plate geometry parameters, in-plane load condition, stiffener-plate cross-section area ratio and stiffness ratio on the static and dynamic behaviors of curvilinearly stiffened plate are investigated. Results have shown that behavior of the natural frequency parameter as a function of applied in-plane stress could be affected by the plate thickness, in-plane load condition, stiffener-plate cross-section area ratio and stiffness ratio during compression only, but not when subjected to in-plane tension.
UR - http://www.scopus.com/inward/record.url?scp=84937952620&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84937952620
T3 - 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
BT - 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015
Y2 - 5 January 2015 through 9 January 2015
ER -