=+55. Failures in aircraft gas turbine engines due to high cycle fatigue is a pervasive problem. The

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=+55. Failures in aircraft gas turbine engines due to high cycle fatigue is a pervasive problem. The article

“Effect of Crystal Orientation on Fatigue Failure of Single Crystal Nickel Base Turbine Blade Superalloys” (J. of Engr. for Gas Turbines and Power, 2002:

161–176) gave the accompanying data and fit a nonlinear regression model in order to predict strain

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Applied Statistics For Engineers And Scientists

ISBN: 9781133111368

3rd Edition

Authors: Jay L. Devore, Nicholas R. Farnum, Jimmy A. Doi

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