Buckling of Laminated Composite Stiffened Panels Subjected to Linearly Varying In-Plane Edge Loading
Author:
Publisher
Informa UK Limited
Subject
Computational Mathematics,Computational Mechanics
Link
http://www.tandfonline.com/doi/pdf/10.1080/15502287.2013.834000
Reference14 articles.
1. A Review of Laminated Composite Plate Buckling
2. Closed-form buckling analysis of stiffened composite plates and identification of minimum stiffener requirements
3. Optimum design of FRP box-girder bridges
4. Timoshenko , S. P. and Gere , J. M. 1961.Theory of Elastic Stability,,2nd ed., 373–379. New York: McGraw Hill.
5. Exact solutions for the buckling of rectangular plates having linearly varying in-plane loading on two opposite simply supported edges
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1. A review on buckling of the laminated composite panel under in-plane load;Engineering Research Express;2024-04-04
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3. Buckling and vibration analysis of shape memory laminated composite beams under axially heterogeneous in-plane loads in the glass transition temperature region;SN Applied Sciences;2021-03-12
4. Influence of dynamic temperature variation and inplane varying loads over post-buckling and free vibration analysis of sandwich composite beam;International Journal of Computational Materials Science and Engineering;2020-09
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