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Stress intensity factors for long, deep surface flaws in plates under extensional fieldsUsing a singular solution for a part circular crack, a Taylor Series Correction Method (TSCM) was verified for extracting stress intensity factors from photoelastic data. Photoelastic experiments were then conducted on plates with part circular and flat bottomed cracks for flaw depth to thickness ratios of 0.25, 0.50 and 0.75 and for equivalent flaw depth to equivalent ellipse length values ranging from 0.066 to 0.319. Experimental results agreed well with the Smith theory but indicated that the use of the ''equivalent'' semi-elliptical flaw results was not valid for a/2c less than 0.20. Best overall agreement for the moderate (a/t approximately 0.5) to deep flaws (a/t approximatelly 0.75) and a/2c greater than 0.15 was found with a semi-empirical theory, when compared on the basis of equivalent flaw depth and area.
Document ID
19730015188
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Harms, A. E.
(Virginia Polytechnic Inst. Blacksburg, VA, United States)
Smith, C. W.
(Virginia Polytechnic Inst. Blacksburg, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1973
Subject Category
Structural Mechanics
Report/Patent Number
VPI-E-73-6
NASA-CR-132015
Report Number: VPI-E-73-6
Report Number: NASA-CR-132015
Accession Number
73N23915
Funding Number(s)
CONTRACT_GRANT: NGR-47-004-076
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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