0
TECHNICAL PAPERS

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
Your Session has timed out. Please sign back in to continue.

References

Reddy,  J. N., and Phan,  N. D., 1985, “Stability and Vibration of Isotropic. Orthotropic and Laminated Plates According to a Higher-Order Shear Deformation Theory,” J. Sound Vib., 98, pp. 157–170.
Reddy,  J. N., 1984, “A Simple Higher-Order Theory for Laminated Composite Plates,” ASME J. Appl. Mech., 51(4), pp. 745–752.
Senthilnathan,  N. R., Lim,  S. P., Lee,  K. H., and Chow,  S. T., 1987, “Buckling of Shear Deformable Plates,” AIAA J., 25, pp. 1268–1271.
Khdeir,  A. A., 1988, “Free Vibration and Buckling of Symmetric Cross-Ply Laminated Plates by an Exact Method,” J. Sound Vib., 126, pp. 447–461.
Khdeir,  A. A., 1989, “Stability of Anti-Symmetric Angle-Ply Laminated Plates,” J. Eng. Mech., 115, pp. 952–962.
Doong,  J. L., 1987, “Vibration and Stability of an Initially Stressed Thick Plate According to a Higher-Order Deformation Theory,” J. Sound Vib., 113, pp. 425–440.
Doong,  J. L., Lee,  C., and Fung,  C. P., 1991, “Vibration and Stability of Laminated Plates Based on a Modified Plate Theory,” J. Sound Vib., 151, pp. 193–201.
Ren,  J. G., and Owen,  D. R. J., 1989, “Vibration and Buckling of Laminated Plates,” Int. J. Solids Struct., 25, pp. 95–106.
Savithri,  S., and Varadhan,  T. K., 1990, “Free Vibration and Stability of Cross-Ply Laminated Plates,” J. Sound Vib., 141, pp. 516–520.
Matsunaga,  H., 2000, “Vibration and Stability of Cross-Ply Laminated Composite Plates According to a Global Higher-Order Plate Theory,” Compos. Struct., 48, pp. 234–244.
Kant,  T., and Swaminathan,  K., 2000, “Analytical Solutions Using a Higher Order Refined Theory for The Stability Analysis of Laminated Composite and Sandwich Plates,” Struct. Eng. Mech., 10(4), pp. 337–357.
Pagano,  N. J., 1969, “Exact Solutions for Composite Laminates in Cylindrical Bending,” J. Compos. Mater., 3, pp. 398–411.
Pagano,  N. J., 1970, “Exact Solutions for Rectangular Bi-Directional Composites,” J. Compos. Mater., 4, pp. 20–34.
Wu,  C. P., and Chen,  W. Y., 1994, “Vibration and Stability of Laminated Plates Based on a Local High Order Plate Theory,” J. Sound Vib., 177(4), pp. 503–520.
Narita,  Y., and Leissa,  A. W., 1990, “Buckling Studies for Simply Supported Symmetrically Laminated Rectangular Plates,” Int. J. Mech. Sci., 32(11), pp. 909–924.
Srinivas, S., 1970, “Three-Dimensional Analysis of Some Plates and Laminates and a Study of Thickness Effects,” Ph.D. thesis, Department of Aeronautical Engineering, Indian Institute of Science Banglore, India.
Srinivas,  S., and Rao,  A. K., 1970, “Bending, Vibration and Buckling of Simply Supported Thick Orthotropic Rectangular Plates and Laminates,” Int. J. Solids Struct., 6, pp. 1463–1481.
Noor,  A. K., 1975, “Stability of Multilayered Composite Plates,” Fibre Sci. Technol., 8(2), pp. 81–89.
Putcha,  N. S., and Reddy,  J. N., 1986, “Stability and Natural Vibration Analysis of Laminated Plates by Using a Mixed Element Based on a Refined Plate Theory,” J. Sound Vib., 104(2), pp. 285–300.
Noor,  A. K., and Burton,  W. S., 1992, “Three-Dimensional Solutions for Thermal Buckling of Multilayered Anisotropic Plates,” J. Eng. Mech., 118(4), pp. 683–701.
Sai Ram,  K. S., and Sinha,  P. K., 1992, “Hygro-Thermal Effects on the Buckling of Laminated Composite Plates,” Compos. Struct., 21, pp. 233–247.

Figures

Grahic Jump Location
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
Grahic Jump Location
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
Grahic Jump Location
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
Grahic Jump Location
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

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In