Creep-age forming of AA7475 aluminum panels for aircraft lower wing skin application
Author:
Affiliation:
1. Empresa Brasileira de Aeronáutica S.A., Brasil
2. Universidade Federal de São Paulo, Brasil
Publisher
FapUNIFESP (SciELO)
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science
Link
http://www.scielo.br/pdf/mr/v15n4/aop_1074-11.pdf
Reference12 articles.
1. Autoclave age forming large aluminum aircraft panels;Holman MC;Journal of Mechanical Working Technology.,1989
2. A simple unified age forming model;Narimetla SP;Materials Research Communications,2000
3. Constitutive modelling of primary creep for age forming an aluminium alloy;Ho KC;Journal of Materials Processing Technology,2004
4. A closed form technique to predict springback in creep age-forming;Jeunechamps PP;International Journal of Mechanical,2006
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