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Determination of Design Data for Heat Treated Titanium Alloy Sheet

其他書名	Test techniques and results for creep and fatigue. Volume 2b
出版	Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962
URL	http://books.google.com.hk/books?id=RE_VcoWKvGkC&hl=&source=gbs_api

註釋Mechanical and physical property data, necessary to fulfill the requirements of Phase II of the Department of Defense Titanium Alloy Sheet Rolling Program, were obtained for selected solution treated and aged titanium alloys in sheet form. Four alloys were investigated: BI20VCA, (Ti-13V-11Cr-3Al), Ti-6Al-4v, Ti-2.5Al-16V, and Ti-4Al-3Mo-1V. They were suppled by the producers in the heat treated condtion from fhree or more heats and three thicknesses of each alloy. Static mechanical property data for tension, compression, bearing, shear and crippling; creep and rupture data for tension, compression, bearing and shear; and axial-load fatigue data were obtained at room and elevated temperatures. Fastener and weld joint data from -320F to 80F and physical properties from -420F to 1200F were obtained. Volume 2b contains procedures and results for creep and fatigue tests.