You are being redirected because this document is part of your ASTM Compass® subscription.
    This document is part of your ASTM Compass® subscription.


    Analysis of Circumferential Cracks in Circular Cylinders Using the Weight-Function Method

    Published: 0

      Format Pages Price  
    PDF (384K) 24 $25   ADD TO CART
    Complete Source PDF (20M) 856 $214   ADD TO CART


    Circumferential cracks in hollow circular cylinders are often used as idealizations of flaws in weldments caused by lack of penetration. The most common cases occur for butt welds in pipes, nozzles, and cylindrical pressure vessels. The objective of the present work is to develop a methodology to compute accurately values of stress intensity factor for the entire range of radius ratio, Ri/Ro (inner to outer), from 0 to 0.9999 and crack-depth-to-thickness ratio, a/t, from 0 to 1.0 for general loading using the weight-function approach. The p-version of the finite-element method was used to obtain stress intensity factors and crack face displacements for the reference loading of uniform tension. The reference solution was obtained for selected values of the geometrical parameters, Ri/Ro and a/t, covering their whole range. Both internal and external cracks were treated. Piecewise cubic Hermite interpolation techniques were then used to compute the quantities corresponding to intermediate values of the geometrical parameters. The derivatives of crack face displacements needed in the weight function method were obtained numerically from a three-term Williams series fit to the displacements obtained from the finite-element analysis. The results obtained were compared to existing solutions for uniform tension loading and excellent agreement was found. Results for uniform tension loading obtained from the weight function method were compared with those from finite-element analysis and error bounds were established.


    fracture mechanics, circumferential cracks, hollow cylinder, pipes, weight function, stress intensity factor, p, -version finite element, axisymmetric loading, fatigue (materials)

    Author Information:

    Mettu, SR
    Advanced systems engineering specialist, Lockheed Engineering and Sciences Company, Houston, TX

    Forman, RG
    Senior materials engineer, NASA Lyndon B. Johnson Space Center, Houston, TX

    Committee/Subcommittee: E08.08

    DOI: 10.1520/STP24281S