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NASA NTRS · 19730015188

Stress intensity factors for long, deep surface flaws in plates under extensional fields

Abstract

Using 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.

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BibTeXRIS

Harms, A. E., Smith, C. W.. 1973-02-01. Stress intensity factors for long, deep surface flaws in plates under extensional fields. https://ntrs.nasa.gov/citations/19730015188

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