Fatigue and Corrosion-Fatigue Crack Propagation in Intermediate-Strength Aluminum Alloys

dc.contributor.author	T. W. Crooker
dc.date.accessioned	2017-05-09T01:36:25Z
dc.date.available	2017-05-09T01:36:25Z
dc.date.copyright	July, 1973
dc.date.issued	1973
dc.identifier.issn	0094-4289
dc.identifier.other	JEMTA8-26833#150_1.pdf
dc.identifier.uri	http://yetl.yabesh.ir/yetl/handle/yetl/163814
dc.description.abstract	Fatigue crack propagation studies were conducted on a variety of intermediate-strength aluminum alloys under high stress-intensity range cycling (ΔK > 10 ksiin.). Tests were conducted in ambient room air and in 3.5-percent NaCl saltwater environments. Data are presented on log-log coordinates in terms of fatigue crack growth rate (da/dN) as a function of the stress-intensity factor range (ΔK). Comparisons are made among similar crack propagation data for steel and titanium alloys.
dc.publisher	The American Society of Mechanical Engineers (ASME)
dc.title	Fatigue and Corrosion-Fatigue Crack Propagation in Intermediate-Strength Aluminum Alloys
dc.type	Journal Paper
dc.journal.volume	95
dc.journal.issue	3
dc.journal.title	Journal of Engineering Materials and Technology
dc.identifier.doi	10.1115/1.3443142
dc.journal.fristpage	150
dc.journal.lastpage	156
dc.identifier.eissn	1528-8889
dc.keywords	Fatigue
dc.keywords	Aluminum alloys
dc.keywords	Corrosion
dc.keywords	Crack propagation
dc.keywords	Fatigue cracks
dc.keywords	Stress
dc.keywords	Titanium alloys AND Steel
dc.tree	Journal of Engineering Materials and Technology:;1973:;volume( 095 ):;issue: 003
dc.contenttype	Fulltext