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RESEARCH PAPERS

Mode II Fatigue Crack Propagation

[+] Author and Article Information
R. Roberts

Lehigh University, Bethlehem, Pa.

J. J. Kibler

Solid Mechanics Laboratory, Re-entry and Environmental Systems Division, General Electric Co., Schenectady, N. Y.

J. Basic Eng 93(4), 671-680 (Dec 01, 1971) (10 pages) doi:10.1115/1.3425325 History: Received November 30, 1970; Online October 27, 2010

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.

Copyright © 1971 by ASME
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