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Keywords: remaining life assessment
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Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. April 2006, 128(2): 240–250.
Published Online: February 1, 2005
... for the design. During the creep run, most of the external points in the airfoil experience stress relaxation, while inner rib points inside the airfoil experience a state of overstress. This is illustrated in Figs. 11 12 . 01 10 2004 01 02 2005 remaining life assessment gas turbines...