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HIGH-ORDER ELEMENT FOR PREBUCKLING AND BUCKLING ANALYSIS OF LAMINATED PLANE FRAMES

✍ Scribed by I. SHEINMAN; M. EISENBERGER; Y. BERNSTEIN


Publisher
John Wiley and Sons
Year
1996
Tongue
English
Weight
559 KB
Volume
39
Category
Article
ISSN
0029-5981

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✦ Synopsis


A new high-order element for prebuckling and buckling of any laminated plane frame is developed. The kinematic approach involves a variety of high-order models with different powers of the thickness coordinate, and the derived stiffness matrix is based on a special power series, without a numerical process. It yields an exact formulation for high-order (first) models and improved formulations for higher-order (second and third) ones. A parametric study of the 'locking' phenomenon and the shear deformation effects was camed out for isotropic and laminated structures. It was found that the first-order model with an appropriate shear correction factor yielded results close to its higher-order counterparts.


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Load increment procedure for post-buckli
✍ S. S. E. Lam; G. P. Zou πŸ“‚ Article πŸ“… 2000 πŸ› John Wiley and Sons 🌐 English βš– 159 KB πŸ‘ 2 views

A load increment procedure has been presented to integrate with the ΓΏnite strip method for the post-buckling analysis of laminated plates when subjected to uniform end shortening. In-plane loads are introduced to re ect the end shortening e ect. The Newton-Raphson procedure is implemented to attend