NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Stress-intensity factors for small surface and corner cracks in platesThree-dimensional finite-element and finite-alternating methods were used to obtain the stress-intensity factors for small surface and corner cracked plates subjected to remote tension and bending loads. The crack-depth-to-crack-length ratios (a/c) ranged from 0.2 to 1 and the crack-depth-to-plate-thickness ratios (a/t) ranged from 0.05 to 0.2. The performance of the finite-element alternating method was studied on these crack configurations. A study of the computational effort involved in the finite-element alternating method showed that several crack configurations could be analyzed with a single rectangular mesh idealization, whereas the conventional finite-element method requires a different mesh for each configuration. The stress-intensity factors obtained with the finite-element-alternating method agreed well (within 5 percent) with those calculated from the finite-element method with singularity elements.
Document ID
19880013061
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Raju, I. S.
(NASA Langley Research Center Hampton, VA., United States)
Atluri, S. N.
(Georgia Inst. of Tech. Atlanta., United States)
Newman, J. C., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1988
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-100599
NAS 1.15:100599
Accession Number
88N22445
Funding Number(s)
PROJECT: RTOP 505-63-01-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available