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contributor authorCraig McClung, R.
contributor authorLee, Yi-Der
contributor authorSobotka, James C.
contributor authorMoody, Jonathan P.
contributor authorBhamidipati, Vikram
contributor authorEnright, Michael P.
contributor authorBenjamin Guseman, D.
contributor authorThomas, Colin B.
date accessioned2019-03-17T09:34:19Z
date available2019-03-17T09:34:19Z
date copyright9/19/2018 12:00:00 AM
date issued2019
identifier issn0742-4795
identifier othergtp_141_02_021005.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4255553
description abstractRecent advances in practical engineering methods for fracture analysis of turbomachinery components are described. A comprehensive set of weight function (WF) stress intensity factor (SIF) solutions for elliptical and straight cracks under univariant and bivariant stress gradients has been developed and verified. Specialized SIF solutions have been derived for curved through cracks, cracks at chamfered and angled corners, and cracks under displacement control. Automated fracture models are available to construct fatigue crack growth (FCG) life contours and critical initial crack size (CICS) contours for all nodal locations in two-dimensional or three-dimensional (2D or 3D) finite element (FE) models.
publisherThe American Society of Mechanical Engineers (ASME)
titleSome Recent Advances in Engineering Fracture Modeling for Turbomachinery
typeJournal Paper
journal volume141
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4040901
journal fristpage21005
journal lastpage021005-9
treeJournal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 002
contenttypeFulltext


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