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contributor authorJ. R. Beisheim
contributor authorG. B. Sinclair
date accessioned2017-05-09T00:11:44Z
date available2017-05-09T00:11:44Z
date copyrightApril, 2003
date issued2003
identifier issn0889-504X
identifier otherJOTUEI-28702#372_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129281
description abstractThe stress analysis of dovetail attachments presents some challenges. These stem from the high stress gradients at the edges of contact. They also stem from the nonlinearities accompanying conforming contact. Even with two-dimensional analysis, obtaining converged peak stresses is not trivial. With three-dimensional analysis, convergence can be expected to be more difficult to achieve because of the added computational costs of refinement in three dimensions. To meet these challenges, this paper describes a submodeling procedure with finite elements. The submodeling approach features bicubic surface fits to displacements for submodel boundary conditions. The approach also features a means of verifying these boundary conditions have converged; this is crucial to obtaining accurate converged peak stresses. The approach is applied to a three-dimensional test piece used to simulate a dovetail attachment. This application leads to converged three-dimensional stresses. These stresses serve to quantify the sort of increases in contact stresses in attachments due to three-dimensional effects.
publisherThe American Society of Mechanical Engineers (ASME)
titleOn the Three-Dimensional Finite Element Analysis of Dovetail Attachments
typeJournal Paper
journal volume125
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1539867
journal fristpage372
journal lastpage379
identifier eissn1528-8900
keywordsStress
keywordsFinite element analysis
keywordsBoundary-value problems
keywordsBlades
keywordsDisks AND Dimensions
treeJournal of Turbomachinery:;2003:;volume( 125 ):;issue: 002
contenttypeFulltext


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