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Analysis of surface cracks in finite plates under tension or bending loadsStress-intensity factors calculated with a three-dimensional, finite-element analysis for shallow and deep semielliptical surface cracks in finite elastic isotropic plates subjected to tension or bending loads are presented. A wide range of configuration parameters was investigated. The ratio of crack depth to plate thickness ranged from 0.2 to 0.8 and the ratio of crack depth to crack length ranged from 0.2 to 2.0. The effects of plate width on stress-intensity variations along the crack front was also investigated. A wide-range equation for stress-intensity factors along the crack front as a function of crack depth, crack length, plate thickness, and plate width was developed for tension and bending loads. The equation was used to predict patterns of surface-crack growth under tension or bending fatigue loads. A modified form of the equation was also used to correlate surface-crack fracture data for a brittle epoxy material within + or - 10 percent for a wide range of crack shapes and crack sizes.
Document ID
19800005257
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Newman, J. C., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Raju, I. S.
(Joint Inst. for the Advancement of Flight Sciences Hampton, Va., United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1979
Subject Category
Structural Mechanics
Report/Patent Number
L-13053
NASA-TP-1578
Report Number: L-13053
Report Number: NASA-TP-1578
Accession Number
80N13512
Funding Number(s)
PROJECT: RTOP 506-53-53-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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