Abstract
The elastic post-buckling behavior of thin plates covers a relatively vast region in which geometry nonlinearity (large deflection) and material linearity (Hooke's low) are realized. In this region, a thin rectangular plate has constant stiffnesses in both orthogonal directions. Few simplified analysis guidelines have been analytically represented for in-plane stiffnesses of an elastic post-buckled thin plate subjected to biaxial loads. In this study, Marguerre's equations (the generalized form of von Karman equations), which describe the elastic post-buckling behavior of imperfect thin plates, are solved. Galerkin's method is used to solve these equations in a semi-analytical procedure. Simply supported imperfect thin rectangular plates are considered, and the stresses and displacements functions are obtained in two orthogonal directions to determine corresponding in-plane stiffnesses of the plate. Also, the maximum applicable load is obtained so that the material's linear behavior is maintained. The semi-analytical procedure has accuracy enough to predict the in-plane stiffness of post-buckled plates and can be easily used for practical purposes.
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Abbreviations
- a :
-
Length of the plate
- \(b\) :
-
Width of the plate
- \(h\) :
-
Thickness of the plate
- \(f\) :
-
Amplitude of the deflection function
- \({f}_{0}\) :
-
Amplitude of the initial imperfection function
- \({f}_{\mathrm{cr}}\) :
-
Amplitude of the deflection function at the beginning of the elastic post-buckling region
- \({f}_{\mathrm{max}}\) :
-
Amplitude of the deflection function at the end of the elastic post-buckling region
- \({f}_{\mathrm{T}}\) :
-
Total amplitude of the deflection function
- \({k}_{x}\) :
-
Elastic buckling coefficient of the plate
- \({\bar{k}}_{x}\) :
-
In-plane stiffness of the plate in the x-direction
- \({\bar{k}}_{y}\) :
-
In-plane stiffness of the plate in the y-direction
- \(m\) :
-
Number of half-waves in the x-direction
- \(n\) :
-
Number of half-waves in the y-direction
- \(u\) :
-
Displacement function in the x-direction
- \(v\) :
-
Displacement function in the y-direction
- \(w\) :
-
Displacement function in the z-direction
- \({w}_{0}\) :
-
Initial imperfection function in the z-direction
- \({w}_{\mathrm{T}}\) :
-
Total displacement function in the z-function
- \(D\) :
-
Flexural rigidity of the plate
- \(E\) :
-
Modulus of elasticity
- \(F\) :
-
Airy's stress function
- \({N}_{x}\) :
-
Applied load in the x-direction
- \({N}_{y}\) :
-
Applied load in the y-direction
- \({N}_{xy}\) :
-
Applied load in the xy-direction
- \(\beta \) :
-
Loads' ratio
- \(\lambda \) :
-
Slenderness ratio of the plate
- \(\mu \) :
-
Poisson's ratio
- \({\sigma }_{\rm e}\) :
-
Stress intensity
- \({\sigma }_{p}\) :
-
Proportional limit stress
- \({\sigma }_{x}\) :
-
Normal stress in the x-direction
- \({\sigma }_{xa}\) :
-
Average stress in the x-direction
- \({\sigma }_{xa,\mathrm{max}}\) :
-
Average stress in the x-direction at the end of the elastic post-buckling region
- \({\sigma }_{x,\mathrm{cr}}\) :
-
Elastic buckling stress in the x-direction
- \({\sigma }_{y}\) :
-
Normal stress in the y-direction
- \({\sigma }_{ya}\) :
-
Average stress in the y-direction
- \({\sigma }_{\mathrm{yeild}}\) :
-
Yield stress of the plate material
- \(\phi \) :
-
Aspect ratio of the plate
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Jahanpour, A., Ahmadvand-Shahverdi, F. In-plane stiffness of imperfect thin rectangular plates subjected to biaxial loads in elastic post-buckling region. Arch Appl Mech 91, 2973–2989 (2021). https://doi.org/10.1007/s00419-021-01943-z
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DOI: https://doi.org/10.1007/s00419-021-01943-z