Development and Validation of an S-N Based Two Phase Bending Fatigue Life Prediction Model

Author:

Singh Avinash1

Affiliation:

1. Advanced Power Transfer, GM Powertrain, General Motors Corporation, Wixom, MI 48393

Abstract

The stress-life S-N method along with the Palmgren-Miner cumulative damage theory is the simplest and the most commonly used fatigue life prediction technique. Its main advantage is that the material properties needed are easy to collect and life calculation is simple. However under many variable amplitude loading conditions, life predictions have been found to be unreliable. Various modifications have been proposed to the Palmgren-Miner theory, but they have not lead to more reliable life predictions. In this paper, a two-stage cumulative damage model will be developed and validated. This model divides fatigue life into two phases—a crack initiation phase and a crack propagation phase. It will be shown that the proposed method results in greatly improved life prediction capabilities. Also, the proposed method retains the simplicity of the S-N based approach in that the material data is still relatively simple to generate and the calculations are straightforward.

Publisher

ASME International

Subject

Computer Graphics and Computer-Aided Design,Computer Science Applications,Mechanical Engineering,Mechanics of Materials

Reference7 articles.

1. Corten, H. T., and Dolan, T. J., 1956, “Cumulative Fatigue Damage,” Proc. of the International Conference on Fatigue of Metals, Institute of Mechanical Engineers, London, pp. 235–245.

2. Haibach, E., “Modifizierte lineare Schadenakkumulationshypothese zur Berucksichtigung des Dauerfestigkeitsabfalls mit fortschreitender Schadigung,” Technische Mitteilungen No. 50/70 der Lab. Fur Betriebsfestigkeit, Darmstadt, Germany.

3. Grover, H. J., 1960, “An Observation Concerning the Cycle Ratio in Cumulative Damage,” Fatigue in Aircraft Structures, STP-274, American Society for Testing and Materials, Philadelphia, pp. 120–124.

4. Manson, S. S. , 1966, “Interfaces between Fatigue, Creep, and Fracture,” Int. J. Fract. Mech., 2, pp. 327–363.

5. Manson, S. S., Frecke, J. C., and Ensign, C. R., 1967, “Applications of a Double Linear Damage Rule to Cumulative Fatigue,” Fatigue Crack Propagation, STP-415, American Society for Testing and Materials, Philadelphia, p. 384.

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