Articles liés à Fatigue Life Analysis of MIG Welded 5052-O & 6061-T6...
Synopsis
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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- ÉditeurLAP LAMBERT Academic Publishing
- Date d'édition2020
- ISBN 10 620256430X
- ISBN 13 9786202564304
- ReliureBroché
- Langueanglais
- Nombre de pages56
- Coordonnées du fabricantnon disponible
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Fatigue Life Analysis of MIG Welded 5052-O & 6061-T6 Aluminum Alloys
Edité par
LAP LAMBERT Academic Publishing, 2020
ISBN 10 : 620256430X
ISBN 13 : 9786202564304
Neuf
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Vendeur : moluna, Greven, Allemagne
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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 réf. du vendeur 385947680
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Fatigue Life Analysis of MIG Welded 5052-O & 6061-T6 Aluminum Alloys
Edité par
LAP LAMBERT Academic Publishing Mai 2020, 2020
ISBN 10 : 620256430X
ISBN 13 : 9786202564304
Neuf
Taschenbuch
Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne
Évaluation du vendeur 5 sur 5 étoiles
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 réf. du vendeur 9786202564304
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Fatigue Life Analysis of MIG Welded 5052-O & 6061-T6 Aluminum Alloys
Edité par
LAP LAMBERT Academic Publishing, 2020
ISBN 10 : 620256430X
ISBN 13 : 9786202564304
Neuf
Taschenbuch
Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne
Évaluation du vendeur 5 sur 5 étoiles
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 réf. du vendeur 9786202564304
Quantité disponible : 1 disponible(s)
Image fournie par le vendeur
Fatigue Life Analysis of MIG Welded 5052-O & 6061-T6 Aluminum Alloys
Edité par
LAP LAMBERT Academic Publishing Mai 2020, 2020
ISBN 10 : 620256430X
ISBN 13 : 9786202564304
Neuf
Taschenbuch
Vendeur : buchversandmimpf2000, Emtmannsberg, BAYE, Allemagne
Évaluation du vendeur 5 sur 5 étoiles
Taschenbuch. Etat : Neu. 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.Books on Demand GmbH, Überseering 33, 22297 Hamburg 56 pp. Englisch. N° de réf. du vendeur 9786202564304
Quantité disponible : 2 disponible(s)