Abstract

In a typical structural application of a composite, multiple layers (or laminae) of unidirectional composites are stacked together at various angles to form a laminate. The stacking sequence and orientations of the individual layers give the laminate designer additional ‘degrees of freedom’ to ‘tailor’ or optimize the design with respect to strength, stiffness, buckling load, vibration response, panel flutter or other desired performance objective.

Keywords

Individual Layer Unit Width Classical Lamination Theory Symmetric Laminate Panel Flutter 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

  1. 1.
    Reissner, E. and Stavsky, Y, “Bending and Stretching of Certain Types of Heterogeneous Aeolotropic Elastic Plates,” ASME J. Appl. Mech., 28, 402–408 (1961),Google Scholar
  2. 2.
    Tsai, S. W., “Structural Behavior of Composite Materials,” NASA CR-71 (July 1964).Google Scholar
  3. 3.
    Bert, C.W., “Analysis of Plates,” Composite Materials, ed. L.J. Broutman and R.H. Krock, Academic Press Network, Vol. 7: Structural Design and Analysis, Part I, ed. C.C. Chamis, Ch.4, 149–206 (1975).Google Scholar
  4. 4.
    Bert, C. W., “Optimal Design of a Composite-Material Plate to Maximize Its Fundamental Frequency,” Journal of Sound and Vibration, 50, 229–237 (1977).CrossRefGoogle Scholar
  5. 5.
    Bert, C. W., “Simplified Prediction of Ply Steer in Radial Tires,” Tire Sci. and Tech., 8, 3–9 (1980).CrossRefGoogle Scholar
  6. 6.
    Werren, F. and Norris, C.B., “Mechanical Properties of a Laminate Designed to be Isotropic,” Forest Products Laboratory, Madison, WI, Rep. No. 1841 (1953).Google Scholar
  7. 7.
    Whitney, J.M. and Pagano, N.J., “Shear Deformation in Heterogeneous Anisotropic Plates,” ASME J. Appl. Mech., 37, 1031–1036 (1970).CrossRefGoogle Scholar
  8. 8.
    Whitney, J.M., Structural Analysis of Laminated Anisotropic Plates, Technomic, Lancaster, PA, Ch. 10 (1987).Google Scholar
  9. 9.
    Chia, C. Y., Nonlinear Analysis of Plates, McGraw-Hill, New York, Ch. 5 and 7 (1980).Google Scholar
  10. 10.
    Bert, C. W. and Reddy, J.N., “Bending of Thick Rectangular Plates Laminated of Bimodulus Composite Materials,” AIAA Journal 19, 1342–1349 (1981).CrossRefGoogle Scholar

Copyright information

© Society for Experimental Mechanics 1989

Authors and Affiliations

  • Charles W. Bert

There are no affiliations available

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