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Cyclic Crack Growth Analysis for Notched Structures at Elevated Temperatures

RM. GamblePC. Paris

出版	ASTM International, 1976
URL	http://books.google.com.hk/books?id=a_h6zgEACAAJ&hl=&source=gbs_api

註釋

Linear elastic fracture mechanics analysis in conjunction with the appropriate experimental crack growth data were used to predict allowable thermal fatigue crack growth rates in gas turbine disks. The crack growth predictions made for the turbine disks compared favorably with subsequent service data.