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 |