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Improved stress-intensity factors for semi-elliptical surface cracks in finite-thickness platesStress-intensity factors for shallow and deep semi-elliptical surface cracks in plates subjected to tension are presented. To verify the accuracy of the three-dimensional finite-element models employed, convergence was studied by varying the number of degrees of freedom in the models from 1500 to 6900. The 6900 degrees of freedom used here were more than twice the number used in previously reported solutions.
Document ID
19770020483
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Raju, I. S.
(NASA Langley Research Center Hampton, VA, United States)
Newman, J. C., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1977
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-72825
Report Number: NASA-TM-X-72825
Meeting Information
Meeting: Intern. Conf. on Structural Mechanics in Reactor Technol.
Location: San Francisco
Start Date: August 15, 1977
End Date: August 19, 1977
Accession Number
77N27427
Funding Number(s)
PROJECT: RTOP 505-02-31-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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