A new vibration-based fatigue testing methodology for assessing high-cycle turbine engine material fatigue strength at various stress ratios is presented. The idea is to accumulate fatigue energy on a base-excited plate specimen at high frequency resonant modes and to complete a fatigue test in a much more efficient way at very low cost. The methodology consists of (1) a geometrical design procedure, incorporating a finite-element model to characterize the shape of the specimen for ensuring the required stress state/pattern; (2) a vibration feedback empirical procedure for achieving the high-cycle fatigue experiments with variable-amplitude loading; and finally (3) a pre-strain procedure for achieving various uniaxial stress ratios. The performance of the methodology is demonstrated with experimental results for mild steel, 6061-T6 aluminum, and Ti-6Al-4V plate specimens subjected to a fully reversed bending, uniaxial stress state.
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e-mail: shen.1@osu.edu
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January 2005
Technical Papers
Goodman Diagram Via Vibration-Based Fatigue Testing
Tommy J. George,
Tommy J. George
Air Force Research Laboratory, Wright-Patterson AFB, OH 45433
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M.-H. Herman Shen,
e-mail: shen.1@osu.edu
M.-H. Herman Shen
Department of Mechanical Engineering, The Ohio State University, Columbus, OH 43210
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Onome Scott-Emuakpor,
Onome Scott-Emuakpor
Department of Mechanical Engineering, The Ohio State University, Columbus, OH 43210
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Theodore Nicholas,
Theodore Nicholas
Air Force Institute of Technology, Wright-Patterson AFB, OH 45433
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Charles J. Cross,
Charles J. Cross
Air Force Research Laboratory, Wright-Patterson AFB, OH 45433
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Jeffrey Calcaterra
Jeffrey Calcaterra
Air Force Research Laboratory, Wright-Patterson AFB, OH 45433
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Tommy J. George
Air Force Research Laboratory, Wright-Patterson AFB, OH 45433
M.-H. Herman Shen
Department of Mechanical Engineering, The Ohio State University, Columbus, OH 43210
e-mail: shen.1@osu.edu
Onome Scott-Emuakpor
Department of Mechanical Engineering, The Ohio State University, Columbus, OH 43210
Theodore Nicholas
Air Force Institute of Technology, Wright-Patterson AFB, OH 45433
Charles J. Cross
Air Force Research Laboratory, Wright-Patterson AFB, OH 45433
Jeffrey Calcaterra
Air Force Research Laboratory, Wright-Patterson AFB, OH 45433
Manuscript received January 1, 2003; revision received September 14, 2004. Review conducted by: W. Soboyejo.
J. Eng. Mater. Technol. Jan 2005, 127(1): 58-64 (7 pages)
Published Online: February 22, 2005
Article history
Received:
January 1, 2003
Revised:
September 14, 2004
Online:
February 22, 2005
Citation
George, T. J., Shen, M. H., Scott-Emuakpor, O., Nicholas, T., Cross , C. J., and Calcaterra, J. (February 22, 2005). "Goodman Diagram Via Vibration-Based Fatigue Testing ." ASME. J. Eng. Mater. Technol. January 2005; 127(1): 58–64. https://doi.org/10.1115/1.1836791
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