Researches Regarding Improvement of the Fatigue Limit by Heat Treatments of the Al-Alloys for Aeronautics Industry

dc.contributor.author	Doniga, Ana
dc.contributor.author	Vasilescu, Elisabeta
dc.contributor.author	Istrate, Miltiade
dc.contributor.author	Vasilescu, Ioan
dc.contributor.author	Măcuță, Silviu
dc.date.accessioned	2018-10-09T12:30:14Z
dc.date.available	2018-10-09T12:30:14Z
dc.date.issued	2005
dc.identifier.issn	1453 – 083X
dc.identifier.uri	http://10.11.10.50/xmlui/handle/123456789/5484
dc.description	The Annals of "Dunarea de Jos" University of Galati Fascicle IX Metallurgy and Materials Science ISSN 1453 – 083X NR 1 – 2005	ro_RO
dc.description.abstract	The laboratory experiments were made on the two aluminium alloyed qualities used for aeronautical industry. The structure and mechanical characteristics were analyzed and the gotten results were compared using those two types of the thermal treatments. Also, the conventional thermal treatment was used, consisting of the solution quenching and artificial heat ageing, mode in more working condition. A significantly improvement of the mechanical characteristics was ascertained to the thermical treated test-specimen.	ro_RO
dc.language.iso	en	ro_RO
dc.publisher	Universitatea "Dunărea de Jos" din Galați	ro_RO
dc.subject	thermomechanical treatment	ro_RO
dc.subject	aluminium alloy	ro_RO
dc.title	Researches Regarding Improvement of the Fatigue Limit by Heat Treatments of the Al-Alloys for Aeronautics Industry	ro_RO
dc.type	Article	ro_RO