NASA NTRS · 19720032127
Mode II fatigue crack propagation.
Abstract
Fatigue crack propagation rates were obtained for 2024-T3 bare aluminum plates subjected to in-plane, mode I, extensional loads and transverse, mode II, bending loads. These results were compared to the results of Iida and Kobayashi for in-plane mode I-mode II extensional loads. The engineering significance of mode I-mode II fatigue crack growth is considered in view of the present results. A fatigue crack growth equation for handling mode I-mode II fatigue crack growth rates from existing mode I data is also discussed.
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Roberts, R., Kibler, J. J.. 1971-12-01. Mode II fatigue crack propagation.. https://ntrs.nasa.gov/citations/19720032127
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