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Local fracture mechanics analysis of stringer pull-off and delamination in a post-buckled compression panel
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Whistler, British Columbia, 14-18 August
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A virtual crack-closure technique for calculating stress intensity factors for cracked three dimensional bodies
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Using a mixed mode fatigue delamination criterion
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Prediction of energy release rate for edge delamination using a crack tip element
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Fatigue delamination onset prediction in tapered composite laminates
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Damage prediction in cross-plied curved composite laminates
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Martin, R. H. and Jackson, W. C. Damage prediction in cross-plied curved composite laminates. In Composite Materials: Fatigue and Fracture (Eds W. W. Stinchcomb and N. E. Ashbaugh), ASTM STP 1156, 1993, Vol. 4, pp. 105-126 (American Society for Testing and Materials, Philadelphia, Pennsylvania).
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Mode II fracture toughness evaluation using a four point bend end notched flexure test
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A general sublaminate analysis method for determining strain energy release rates
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American Institute of Aeronautics and Astronautics, Washington, DC
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Flanagan, G. A general sublaminate analysis method for determining strain energy release rates. AIAA paper 94-1356-CP, American Institute of Aeronautics and Astronautics, Washington, DC, 1994.
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