Fatigue Life Analysis of MIG Welded 5052-O & 6061-T6 Aluminum Alloys - Couverture souple

Gupta, Saurabh Kumar

9786202564304: Fatigue Life Analysis of MIG Welded 5052-O & 6061-T6 Aluminum Alloys

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ISBN 10 : 620256430X ISBN 13 : 9786202564304

Editeur : LAP LAMBERT Academic Publishing, 2020

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Steel followed by aluminum alloys are the most frequently welded metal, while some metals cannot be effectively welded. In this work, two different aluminum alloys AA5052-O and AA6061-T6 are joined by MIG welding. Then compared the fatigue life of welded specimen at different loading conditions such as constant amplitude loading, constant amplitude loading with Intermediate single overload, variable amplitude loading. It has been found that welded AA6061-T6 alloy has more life than welded AA5052-O aluminum alloy. Fatigue life of welded alloy 6061-T6 and 5052-O is greater under block loading than intermediate single overloading.

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�diteur: LAP LAMBERT Academic Publishing
Date d'�dition: 2020
Langue: anglais
ISBN 10: 620256430X
ISBN 13: 9786202564304
Reliure: Broch�
Nombre de pages: 56
Coordonn�es du fabricant: non disponible
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Fatigue Life Analysis of MIG Welded 5052-O & 6061-T6 Aluminum Alloys

Saurabh Kumar Gupta

Edit� par LAP LAMBERT Academic Publishing Mai 2020, 2020

ISBN 10 : 620256430X ISBN 13 : 9786202564304

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Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne

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Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Steel followed by aluminum alloys are the most frequently welded metal, while some metals cannot be effectively welded. In this work, two different aluminum alloys AA5052-O and AA6061-T6 are joined by MIG welding. Then compared the fatigue life of welded specimen at different loading conditions such as constant amplitude loading, constant amplitude loading with Intermediate single overload, variable amplitude loading. It has been found that welded AA6061-T6 alloy has more life than welded AA5052-O aluminum alloy. Fatigue life of welded alloy 6061-T6 and 5052-O is greater under block loading than intermediate single overloading. 56 pp. Englisch. N� de r�f. du vendeur 9786202564304

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Fatigue Life Analysis of MIG Welded 5052-O & 6061-T6 Aluminum Alloys

Saurabh Kumar Gupta

Edit� par LAP LAMBERT Academic Publishing, 2020

ISBN 10 : 620256430X ISBN 13 : 9786202564304

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Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne

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Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Steel followed by aluminum alloys are the most frequently welded metal, while some metals cannot be effectively welded. In this work, two different aluminum alloys AA5052-O and AA6061-T6 are joined by MIG welding. Then compared the fatigue life of welded specimen at different loading conditions such as constant amplitude loading, constant amplitude loading with Intermediate single overload, variable amplitude loading. It has been found that welded AA6061-T6 alloy has more life than welded AA5052-O aluminum alloy. Fatigue life of welded alloy 6061-T6 and 5052-O is greater under block loading than intermediate single overloading. N� de r�f. du vendeur 9786202564304

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Fatigue Life Analysis of MIG Welded 5052-O & 6061-T6 Aluminum Alloys

Saurabh Kumar Gupta

Edit� par LAP LAMBERT Academic Publishing, 2020

ISBN 10 : 620256430X ISBN 13 : 9786202564304

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Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Gupta Saurabh KumarDr. Saurabh Kumar Gupta is working as an Associate Professor in the Department of Mechanical Engineering, Raj Kumar Goel Institute of Technology, Ghaziabad. He has more than five years teaching experience. He has p. N� de r�f. du vendeur 385947680

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Fatigue Life Analysis of MIG Welded 5052-O & 6061-T6 Aluminum Alloys

Saurabh Kumar Gupta

Edit� par LAP LAMBERT Academic Publishing Mai 2020, 2020

ISBN 10 : 620256430X ISBN 13 : 9786202564304

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Vendeur : buchversandmimpf2000, Emtmannsberg, BAYE, Allemagne

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Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -Steel followed by aluminum alloys are the most frequently welded metal, while some metals cannot be effectively welded. In this work, two different aluminum alloys AA5052-O and AA6061-T6 are joined by MIG welding. Then compared the fatigue life of welded specimen at different loading conditions such as constant amplitude loading, constant amplitude loading with Intermediate single overload, variable amplitude loading. It has been found that welded AA6061-T6 alloy has more life than welded AA5052-O aluminum alloy. Fatigue life of welded alloy 6061-T6 and 5052-O is greater under block loading than intermediate single overloading.VDM Verlag, Dudweiler Landstra�e 99, 66123 Saarbr�cken 56 pp. Englisch. N� de r�f. du vendeur 9786202564304

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