NASA NTRS · 20070017318
Numerical Strip-Yield Calculation of CTOD
Abstract
Many existing methods to calculate CTOD can be costly and complicated, or apply only to particular configurations. A new numerical method for calculating CTOD was investigated. NASGRO's Boundary Element module NASBEM was adapted to calculate displacements at any point on the crack. Demonstrated for a number of crack configurations: a) finite and infinite domains; b) center and edge cracks; and c) complex cases with several cracks and holes. Great accuracy at minimal computational cost.
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Beek, Joachim, Forman, Royce. 2007-04-16. Numerical Strip-Yield Calculation of CTOD. https://ntrs.nasa.gov/citations/20070017318
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