Thermomechanical Buckling of Laminated Composite Plates Using Mixed, Higher-Order Analytical Formulation

[+] Author and Article Information
J. B. Dafedar, Y. M. Desai

  Department of Civil Engineering, Indian Institute of Technology Bombay, Powai, Mumbai 400 076, India

J. Appl. Mech 69(6), 790-799 (Oct 31, 2002) (10 pages) doi:10.1115/1.1490372 History: Received July 11, 2001; Revised December 05, 2001; Online October 31, 2002
Copyright © 2002 by ASME
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Laminated plate geometry, coordinate axes and degrees-of-freedom for (a) ith layer of a laminated plate in conjunction with HYF1 model, (b) laminated plate
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Variation of biaxial buckling load parameter λB with Ly/H for a crossply [0 deg/90 deg/0 deg] laminated plate considered in Example 3
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Variation of normalized (a) transverse normal stress (σzz max); (b) transverse shear stress (τxzxz max); (c) transverse shear stress (τyzyz max); (d) transverse displacement (w/wtop); (e) in-plane stress (σxx max) and (f) in-plane stress (σyy max) for a (0 deg/90 deg/0 deg) crossply laminated plate in Example 3 under bi-axial compressive loading with Px=Py=1
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Effect of moisture change on uni-axial buckling load parameter λU computed by using the HYF13 model for a square [(0/90)s] crossply laminated plate in Example 6




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