In Part I of this paper, the question of the extent of dominance of the mode I asymptotic elastodynamic crack-tip field (the KdI-field) was studied experimentally. Here, the results of two and three-dimensional elastodynamic finite element simulations of the drop-weight experiments are reported. The load records as obtained from the impact hammer and supports of the drop-weight loading device were used as boundary tractions in the numerical simulations. For the laboratory specimen studied, the results of the simulations indicate that the asymptotic elastodynamic field is not an adequate description of the actual fields prevailing over any sizeable region around the crack tip. This confirms the experimental results of Part I which showed that three-dimensional and transient effects necessarily have to be taken into account for valid interpretation of experimental results.
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March 1991
Research Papers
On the Extent of Dominance of Asymptotic Elastodynamic Crack-Tip Fields: Part II—Numerical Investigation of Three-Dimensional and Transient Effects
Sridhav Krishnaswamy,
Sridhav Krishnaswamy
Graduate Aeronautical Laboratories, California Institute of Technology, Pasadena, CA 91125
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Ares J. Rosakis,
Ares J. Rosakis
Graduate Aeronautical Laboratories, California Institute of Technology, Pasadena, CA 91125
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G. Ravichandran
G. Ravichandran
University of California, San Diego, CA
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Sridhav Krishnaswamy
Graduate Aeronautical Laboratories, California Institute of Technology, Pasadena, CA 91125
Ares J. Rosakis
Graduate Aeronautical Laboratories, California Institute of Technology, Pasadena, CA 91125
G. Ravichandran
University of California, San Diego, CA
J. Appl. Mech. Mar 1991, 58(1): 95-103 (9 pages)
Published Online: March 1, 1991
Article history
Received:
March 31, 1989
Revised:
March 14, 1990
Online:
March 31, 2008
Citation
Krishnaswamy, S., Rosakis, A. J., and Ravichandran, G. (March 1, 1991). "On the Extent of Dominance of Asymptotic Elastodynamic Crack-Tip Fields: Part II—Numerical Investigation of Three-Dimensional and Transient Effects." ASME. J. Appl. Mech. March 1991; 58(1): 95–103. https://doi.org/10.1115/1.2897185
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