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Apr 26, 2012

Development of Design Recommendations for Edge-Bolted Laminated Glass

Publication: Structures Congress 2011

Abstract

This paper presents the results of testing and analytical developments sponsored by the U.S. Department of State to provide recommendations for support connection design of through-edge bolted laminated glass. Design equations are presented that capture the capacity of the through-bolted laminate material in reaction to in-plane membrane induced loading. A simple analytical treatment of edge-clamping and tear-out resistance forces is presented. Specific recommendations for bolt pre-load and gasket characteristics are presented. Test data are presented to support the validity of the calculations and recommendations. The various tests were executed by the Force Protection Branch of the Air Force Research Laboratory (AFRL) at Tyndall Air Force Base, Florida and Southern Research Institute in Birmingham, Alabama.

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Go to Structures Congress 2011
Structures Congress 2011
Pages: 1347 - 1358

History

Published online: Apr 26, 2012

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D. Duke, Ph.D. [email protected]
P.E.
M.ASCE
Staff Engineer, Southern Research Institute 757 Tom Martin Drive, Birmingham, AL 35211.E-mail: [email protected]
B. T. Bewick, Ph.D. [email protected]
Research Civil Engineer, Air Force Research Laboratory 139 Barnes Drive, Suite 2, Tyndall AFB, FL 32403.E-mail: [email protected]
MSME, Mechanical Engineer, Southern Research Institute 757 Tom Martin Drive, Birmingham, AL 35211.E-mail: [email protected]
S. R. Misko [email protected]
BSEE, Instrumentation Engineer, Air Force Research Laboratory 104 Research Rd, Bldg 9742, Tyndall AFB, FL 32403.E-mail: [email protected]

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