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contributor authorY. Xiong
date accessioned2017-05-08T23:55:37Z
date available2017-05-08T23:55:37Z
date copyrightSeptember, 1998
date issued1998
identifier issn0021-8936
identifier otherJAMCAV-26450#787_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/119879
description abstractA stress analysis method has been developed for a biaxially loaded fastener hole in a laminated plate of finite geometry. The method is based on a variational formulation involving complex variables. In this method, the equilibrium and compatibility equations are satisfied in the domain of the plate due to the employment of the complex stress potentials and all the boundary conditions are satisfied through a variational statement. Therefore, the requirement for finite width corrections in relatively large fastener hole cases is avoided. The method has been verified through comparison with finite element results.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Stress Analysis Method for Bi-axially Loaded Fastener Hole in Composite Laminate of Finite Geometry
typeJournal Paper
journal volume65
journal issue3
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.2789131
journal fristpage787
journal lastpage790
identifier eissn1528-9036
keywordsComposite materials
keywordsLaminates
keywordsFasteners
keywordsStress analysis (Engineering)
keywordsGeometry
keywordsFinite element analysis
keywordsBoundary-value problems
keywordsEquations
keywordsEquilibrium (Physics) AND Stress
treeJournal of Applied Mechanics:;1998:;volume( 065 ):;issue: 003
contenttypeFulltext


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