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NASA NTRS · 19720017287

Computer analysis of two-dimensional fatigue flaw-growth problems

Abstract

A description is given of a computer program for analyzing the crack propagation in cyclic loaded structures. By using equations for the stress intensity factors for surface and embedded flaws, the capability of ascertaining lengthwise crack growth as well as crack growth through the thickness of the structure was determined. Equations used are written in general form so that many other types of crack growth problems, such as through the thickness type cracks, can be analyzed. Provisions have been made in the computer program to analyze crack growth for repeated blocks of variable-amplitude fatigue load spectra. Additional features of the computer program include a variable print interval and a variable integration interval to minimize computer printout and computer run time. A source listing and instructions for using the computer program are included.

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BibTeXRIS

Forman, R. G., Kavanaugh, H. C., Stuckey, B.. 1972-02-01. Computer analysis of two-dimensional fatigue flaw-growth problems. https://ntrs.nasa.gov/citations/19720017287

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