Prakash, Raghu V and Sunder, R (1993) Fatigue Life Under Random Load History Derived From Exceedance Curves Using Different Algorithms. In: Fatigue & Fracture of Engineering Materials & Structures, 16 (7). pp. 707-721.
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Low cycle fatigue life and crack growth rates were analysis established for random load sequences, generated from three combat aircraft load exceedance curves using different algorithms, including simulated rain-flow cycle count,extreme-to-extreme excursions, upper to lower bound excursions and unrestricted peak-trough excursions. Also, the response of a fatigue meter to a random load sequence was simulated. Fatigue damage for the different load histories was computed using material constants for an Al-Cu alloy. Computed fatigue damage was relatively insensitive to the algorithm used for load sequence generation from combat aircraft load exceedance curves. Fatigue meter data based damage estimates were, however,sometimes unconservative.
| Item Type: | Journal Article |
|---|---|
| Additional Information: | Copyright of this article belongs to John Wiley & Sons, Inc. |
| Department/Centre: | Division of Mechanical Sciences > Mechanical Engineering |
| Date Deposited: | 08 Jul 2008 |
| Last Modified: | 27 Aug 2008 13:33 |
| URI: | http://eprints.iisc.ernet.in/id/eprint/14857 |
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