Abstract

Laminated glass units used for glazing buildings consist of two thin glass plates bonded together by a thin core material, called polyvinyl butyral (PVB). As the plates are usually thin and undergo large lateral displacements, the conventional thin plate theory cannot be applied; instead, a nonlinear theory of plates has to be employed. As well, the interlayer, though soft in material properties, provides significant change in the overall behavior of the composite. Variational calculus and minimum potential energy theorem are employed to obtain the five nonlinear differential equations with appropriate boundary conditions; these equations are solved numerically with iteration. Experiments were conducted at the Glass Research and Testing Laboratory at Texas Tech University, Lubbock, Texas, to validate the mathematical model. Laminated glass units 1.524m×1.524m (60in.×60in.) in size with two glass plates each 4.763 mm (0.1875 in.) thick with a PVB of thickness equal to 1.52 mm (0.06 in.) were tested up to a lateral pressure of 6.895 kPa (1 psi). Lateral displacements and strains at four different locations at the top and bottom of the units were measured. The experimental results are compared with those from the mathematical model and presented in this paper.

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References

1.
Behr, R. A., Minor, J. E., Linden, M. P., and Vallabhan, C. V. G. (1985). “Laminated glass units under uniform lateral pressure.” J. Struct. Engrg., ASCE, 111(5), 1037–1050.
2.
Behr, R. A., and Linden, M. P. (1986). “Load duration and interlayer thickness effects on laminated glass.” J. Struct. Engrg., ASCE, 112(6), 1441–1453.
3.
Das, Y. C., and Vallabhan, C. V. G. (1988). “A mathematical model for nonlinear stress analysis of sandwich plate units.” Math. Comput. Model., 11, 713–719.
4.
Hoff, N. J. (1950). “Bending and buckling of sandwich beams.” Tech. Note 2225. National Advisory Committee for Aeronautics.
5.
Linden, M. P., Minor, J. E., Behr, R. A., and Vallabhan, C. V. G. (1988). Experimental study of laterally loaded laminated glass plates. Glass Research and Testing Laboratory, Texas Tech University, Lubbock, Tex.
6.
Magdi, M. (1990). “Mathematical model for laminated window glass units,” MS thesis, Dept. of Civ. Engrg., Texas Tech. Univ., Lubbock, Tex.
7.
Pister, K. S., and Dong, S. B. (1959). “Elastic bending of layered plates.” J. Engrg. Mech. Div., ASCE, 85(4), 1–10.
8.
Reissner, E. (1948). “Finite defections of sandwich plates.” J. Aeronautic Sci., 15(7),435–440.
9.
Reznik, P. L., and Minor, J. E. (1986). Failure strengths of laminated glass units. Glass Research and Testing Laboratory, Texas Tech University, Lubbock, Tex.
10.
Vallabhan, C. V. G. (1983). “Iterative analysis of nonlinear glass plates.” J. Struct. Engrg., ASCE, 109(2), 2416–2426.
11.
Vallabhan, C. V. G., Minor, J. E., and Nagalla, S. R. (1987). “Stresses in layered glass units and monolithic glass plates.” J. Struct. Engrg., ASCE, 113(1), 36–43.
12.
Wang, C. T. (1952). “Principle and application of complementary energy method for thin homogeneous and sandwich plates and shells with finite defections,” NACA TN 2620. National Advisory Committee on Aeronautics, Washington, D.C.

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Published In

Go to Journal of Structural Engineering
Journal of Structural Engineering
Volume 119Issue 5May 1993
Pages: 1572 - 1585

History

Received: Apr 29, 1991
Published online: May 1, 1993
Published in print: May 1993

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Authors

Affiliations

C. V. Girija Vallabhan, Fellow, ASCE
Prof. Civ. Engrg., Texas Tech Univ., Lubbock, TX 79409
Y. C. Das, Member, ASCE
Assoc. Prof. Civ. Engrg., McNeese State Univ., Lake Charles, LA 70609, U.S.A.
Mohareb Magdi
Grad. Res. Asst., Dept. Civ. Engrg., Texas Tech Univ., Lubbock, TX
Mehmet Asik
Grad. Res. Asst., Dept. Civ. Engrg., Texas Tech Univ., Lubbock, TX
James R. Bailey, Associate Member, ASCE
Res. Engr., Prod. Oper. Div., Exxon Prod. Res. Co., Houston, TX 77252

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