Strain Rate and Loading Waveform Effects on an Energy-Based Fatigue Life Prediction for AL6061-T6

Author:

Letcher Todd1,Shen M.-H. H.2,Scott-Emuakpor Onome,George Tommy,Cross Charles3

Affiliation:

1. e-mail:

2. e-mail:  Mechanical and Aerospace Engineering Department, Building 148, 201 W. 19th Ave., The Ohio State University, Columbus, OH 43210

3. Turbine Engine Fatigue Facility, Air Force Research Laboratory, Wright-Patterson AFB, OH 45433

Abstract

The energy-based lifing method is based on the theory that the cumulative energy in all hysteresis loops of a specimens' lifetime is equal to the energy in a monotonic tension test. Based on this theory, fatigue life can be calculated by dividing monotonic strain energy by a hysteresis energy model, which is a function of stress amplitude. Recent studies have focused on developing this method for a sine wave loading pattern—a variable strain rate. In order to remove the effects of a variable strain rate throughout the fatigue cycle, a constant strain rate triangle wave loading pattern was tested. The testing was conducted at various frequencies to evaluate the effects of multiple constant strain rates. Hysteresis loops created with sine wave loading and triangle loading were compared. The effects of variable and constant strain rate loading patterns on hysteresis loops throughout a specimens' fatigue life are examined.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

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