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Stress analysis method for a clearance fit bolt under bearing loads

Authors :
Crews, J. H., Jr
Naik, R. A
Publication Year :
1985
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1985.

Abstract

In the present, simple analysis method for bolt hole clearance stresses in mechanically fastened joints, an inverse formulation is used with a finite element analysis. Conditions along the bolt hole contact arc are specified by displacement constraint equations. The method was applied to a single fastener clearance-fit joint with typical clearance values, for the cases of a rigid, frictionless bolt and a quasi-isotropic graphite/epoxy laminate. Results indicate that the contact arc, as well as the peak stresses around the hole (and their locations), were strongly influenced by the clearance. After a minor initial nonlinearity, peak stresses varied linearly with applied load. Clearance levels are found to have only a minor influence on overall joint stiffness.

Subjects

Subjects :
Structural Mechanics

Details

Language :
English
Database :
NASA Technical Reports
Publication Type :
Report
Accession number :
edsnas.19850048135
Document Type :
Report