A thermo-mechanical stress prediction improvement of using the classical lamination theory via Saint-Venant’s principle for laminated composite plates-Reference-Cited by-同舟云学术

A thermo-mechanical stress prediction improvement of using the classical lamination theory via Saint-Venant’s principle for laminated composite plates

Published:2018-02 Issue:2 Volume:32 Page:743-752
ISSN:1738-494X
Container-title:Journal of Mechanical Science and Technology
language:en
Short-container-title:J Mech Sci Technol

Author:

Jeong Yong-Min,Kim Jun-Sik

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Link

http://link.springer.com/article/10.1007/s12206-018-0123-3/fulltext.html

Reference23 articles.

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2. W. Yu, J.-S. Kim, D. H. Hodges and M. Cho, A critical evaluation of Reissner-Mindlin type models for composite laminated and sandwich plates, Aerospace Science and Technology, 12 (2008) 408–417.

3. J.-S. Kim, J.-W. Han and M. Cho, Boundary layer state prediction of composite and sandwich plates via an enhanced higher-order shear deformation theory, Composite Structures, 153 (2016) 928–937.

4. J.-W. Han, J.-S. Kim and M. Cho, Generalization of the C0-type zigzag theory for accurate thermomechanical analysis of laminated composites, Composites Part B: Engineering, 122 (2017) 173–191.

5. N. F. Knight Jr. and Y. Qi, Restatement of first-order sheardeformation theory for laminated plates, International Journal of Solids and Structures, 34 (1997) 481–492.

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