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contributor authorHuai Pu Chu
date accessioned2017-05-09T00:20:31Z
date available2017-05-09T00:20:31Z
date copyrightDecember, 1969
date issued1969
identifier issn0098-2202
identifier otherJFEGA4-27348#830_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/134057
description abstractThe notch-bend strength of four titanium, eight aluminum, and eight copper-base alloys was measured. Specimen sizes ranged from 0.4 to 4 in. in section thickness. All materials showed a geometrical size effect on notch strength. Only the high-strength aluminum alloys were found to be prone to brittle fracture. In general, 7Al-2Cb-1Ta titanium, 5456-H321 and 6061-T6 aluminum, and the copper alloys can be considered as notch-tough materials. The titanium alloys exhibited maximum notch toughness with 6–7 percent aluminum content. Determination of plane-strain fracture toughness (KIc ) values for the aluminum alloys is briefly discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Notch-Bend Strength of Titanium, Aluminum, and Copper-Base Alloys in Heavy Sections
typeJournal Paper
journal volume91
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3571227
journal fristpage830
journal lastpage840
identifier eissn1528-901X
keywordsCopper
keywordsAluminum
keywordsAlloys
keywordsTitanium
keywordsToughness
keywordsAluminum alloys
keywordsTitanium alloys
keywordsBrittle fracture
keywordsFracture toughness
keywordsPlane strain
keywordsSize effect
keywordsThickness AND Copper alloys
treeJournal of Fluids Engineering:;1969:;volume( 091 ):;issue: 004
contenttypeFulltext


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