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Fatigue Crack Growth Behavior of Nickel-base Superalloy Haynes 282 at 550-750 °C

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Abstract

The fatigue crack growth rates for nickel-based superalloy Haynes 282 were measured at temperatures of 550, 650, and 750 °C using compact tension specimens with a load ratio of 0.1 and cyclic loading frequencies of 25 Hz and 0.25 Hz. Increasing the temperature from 550 to 750 °C caused the fatigue crack growth rates to increase from ~20 to 60% depending upon the applied stress intensity level. The effect of reducing the applied loading frequency increased the fatigue crack growth rates from ~20 to 70%, also depending upon the applied stress intensity range. The crack path was observed to be transgranular for the temperatures and frequencies used during fatigue crack growth rate testing. At 750 °C, there were some indications of limited intergranular cracking excursions at both loading frequencies; however, the extent of intergranular crack growth was limited and the cause is not understood at this time.

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Abbreviations

R :

Load ratio

P min :

Minimum load

P max :

Maximum load

ΔK :

Stress intensity range

a :

Crack length

W :

Specimen width

B :

Specimen thickness

C p :

Paris constant

m :

Paris slope constant

σ:

Yield strength

E :

Young’s modulus

T :

Temperature

F :

Frequency

da/dN :

The crack growth rate per cycle

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Acknowledgment

This research was supported in part by an appointment to the U.S. Department of Energy (DOE) Postgraduate Research Program at the National Energy Technology Laboratory administered by the Oak Ridge Institute for Science and Education. The authors would also like to thank Dr. Rawley Greene for experimental support and technical programming.

Disclaimer

This report was prepared as an account of work sponsored by an agency of the United States Government. Neither the United States Government nor any agency thereof, nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise does not necessarily constitute or imply its endorsement, recommendation, or favoring by the United States Government or any agency thereof. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States Government or any agency thereof.

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Authors and Affiliations

  1. ORISE, National Energy Technology Laboratory, 1450 Queen Avenue SW, Albany, OR, 97321, USA

    K. A. Rozman

  2. Department of Materials Science, School of Mechanical, Industrial, and Manufacturing Engineering, Oregon State University, Corvallis, OR, 97331, USA

    J. J. Kruzic

  3. National Energy Technology Laboratory, 1450 Queen Avenue SW, Albany, OR, 97321, USA

    J. A. Hawk

Authors
  1. K. A. Rozman
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  2. J. J. Kruzic
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  3. J. A. Hawk
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Correspondence to J. A. Hawk.

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Rozman, K.A., Kruzic, J.J. & Hawk, J.A. Fatigue Crack Growth Behavior of Nickel-base Superalloy Haynes 282 at 550-750 °C. J. of Materi Eng and Perform 24, 2841–2846 (2015). https://doi.org/10.1007/s11665-015-1588-9

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  • DOI: https://doi.org/10.1007/s11665-015-1588-9

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