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[null,"1.","Record Nr.",null,"UNICAMPANIAVAN0250763"]
[null,null,"Autore",null,"Jazar, Reza N."]
[null,null,"Titolo",null,"Perturbation Methods in Science and Engineering / Reza N. Jazar"]
[null,null,"Pubbl/distr/stampa",null,"Cham, : Springer, 2021"]
[null,null,"Descrizione fisica",null,"XVII, 578 p. : ill. ; 24 cm"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,"2.","Record Nr.",null,"UNINA9910346889603321"]
[null,null,"Autore",null,"Hammers Thilo"]
[null,null,"Titolo",null,"Wärmebehandlung und Recken von verbundstranggepressten Luftfahrtprofilen"]
[null,null,"Pubbl/distr/stampa",null,"KIT Scientific Publishing, 2013"]
[null,null,"ISBN",null,"1000031196"]
[null,null,"Descrizione fisica",null,"1 online resource (III, 188 p. p.)"]
[null,null,"Collana",null,"Schriftenreihe des Instituts für Angewandte Materialien, Karlsruher Institut für Technologie"]
[null,null,"Soggetti",null,"Technology: general issues"]
[null,null,"Lingua di pubblicazione",null,"Tedesco"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Sommario/riassunto","Beim Verbundstrangpressen von Luftfahrtprofilen der Legierungen EN AW-6056 und -2099, verstärkt mit Federstahl- oder Kobaltbasisdraht, ist das Verhalten bei Wärmebehandlung und Recken von Interesse. Durch das Strangpressen und die mehrfache Einschnürung des Drahts im Verbund weichen die Verbunde vom Modell ab. Die Grenzfläche wird durch die Wärmebehandlung zum Teil zerstört und beeinflusst so das Verbundverhalten. Eine Lebensdauerprognose der Verbunde unter Ermüdungsbeanspruchung ist möglich."]