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Keywords: Blade Attachment
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Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Tribol. April 2001, 123(2): 413–423.
Published Online: June 27, 2000
... polycrystalline alloys. High cycle fatigue induced failures in aircraft gas turbine and rocket engine turbopump blades is a pervasive problem. Blade attachment regions are prone to fretting fatigue failures. Single crystal nickel base superalloy turbine blades are especially prone to fretting damage because...