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Effects of Design Details on the Fatigue Strength of 355-T6 Sand-cast Aluminum Alloy

Marshall HoltI. D. Eaton

出版	National Advisory Committee for Aeronautics, 1951
URL	http://books.google.com.hk/books?id=E5nmSgAACAAJ&hl=&source=gbs_api

註釋

Data are given on the results of static and fatigue tests of 355-T6 sand-cast plate-type aluminum-alloy specimens incorporating holes, bosses, and ribs.