An alternating method for analysis of surface-flawed aircraft structural components

This publication has 10 references indexed in Scilit:

• Stress-intensity Factors for Two Symmetric Corner Cracks
  Published by ASTM International ,2009
• Analytical solution for embedded elliptical cracks, and finite element alternating method for elliptical surface cracks, subjected to arbitrary loadings
  Engineering Fracture Mechanics, 1983
• Integrity analyses of surface-flawed aircraft attachment lugs - A new, inexpensive, 3-D alternating method
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1982
• 3D analyses of surface flaws in thick-walled reactor pressure-vessels using displacement-hybrid finite element method
  Nuclear Engineering and Design, 1979
• Stress analysis of typical flaws in aerospace structural components using 3-D hybrid displacement finite element method
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1978
• Determination of stress intensity factors for the corner cracked hole using the isoparametric singularity element
  International Journal of Fracture, 1977
• Stress Intensity Factors for Through and Part-Through Cracks Originating at Fastener Holes
  Published by ASTM International ,1976
• Large capacity equation solver for structural analysis
  Computers & Structures, 1974
• Stress intensity factor for an elliptical crack under arbitrary normal loading
  Engineering Fracture Mechanics, 1971
• Numerical Evaluation of Multiple Integrals II
  Mathematical Tables and Other Aids to Computation, 1958