Marshall Technical Reports Server

Development of a Practical Methodology for Elastic-Plastic and Fully Plastic Fatigue Crack Growth

NASA/CR-1999-209428, McClung, R.C. and Chell, G.G. and Lee, Y.D. and Russell*, D.A. and Orient*, G.E., Development of a Practical Methodology for Elastic-Plastic and Fully Plastic Fatigue Crack Growth, Structures and Dynamics Laboratory, Science and Engineering Directorate, Technical Monitor: M. Wayne Gregg, *Subcontract Support from Rocketdyne Division, Boeing North American, 6633 Canoga Ave., Canoga Park, CA 91303, and Southwest Research Institute, P., July, 1999, pp. 485, Format(s): PDF 49836k

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A practical engineering methodology has been developed to analyze and predict fatigue crack growth rates under elastic-plastic and fully plastic conditions. The methodology employs the closure-corrected effective range of the J-integral, Delta J(eff), as the governing parameter. The methodology contains original and literature J and Delta J solutions for specific geometries, along with general methods for estimating J for other geometries and other loading conditions, including combined mechanical loading and combined primary and secondary loading. The methodology also contains specific practical algorithms that translate a J solution into a prediction of fatigue crack growth rate or life, including methods for determining crack opening levels, crack instability conditions, and material properties. A critical core subset of the J solutions and the practical algorithms has been implemented into independent elastic-plastic NASGRO modules. All components of the entire methodology, including the NASGRO modules, have been verified through analysis and experiment, and limits of applicability have been identified
Keywords:elastic-plastic fracture mechanics, elastic-plastic and fully plastic fatigue crack growth, life prediction, j-integral, delta j, finite elements, reference stress method, combined loading, primary and secondary loading, notches, multiaxial, crack closure, crack instability, resistance curves, tear-fatique, creep-fatigue, software, nasgro
Subjects:Engineering: Structural Mechanics: Structural Fatigue
ID Code:473
Deposited On:15 July 2002