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- W2336699402 abstract "AbstractThe aim of this paper is to numerically model the manufacture of aircraft wing panels with double variable curvature and without stringers by creep age forming (CAF) process. The modelling of creep behaviour under uniaxial and ageing condition was performed using both simplified and unified models and compared with literature data for alloy AA7010. A unified model was implemented in MSC.Marc finite elements method program through a subroutine coded in FORTRAN. Then, a methodology was developed to simulate the CAF of an AA7475 aluminium alloy asymmetric panel. The geometry obtained was compared with a real experiment. The uniaxial modelling results show that the simplified model obtained is 46% more exact that the literature model, used as a reference. These results can be improved if the ageing influence on creep is better quantified. The simulation method has described the material behaviour, but there were modelling and experimental limitations that have lead for errors around 20%." @default.
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- W2336699402 date "2016-01-02" @default.
- W2336699402 modified "2023-09-26" @default.
- W2336699402 title "Experimental and numerical modelling and simulation of the creep age forming of aeronautic panels AA7XXX aluminium alloy" @default.
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- W2336699402 doi "https://doi.org/10.1080/2374068x.2016.1147764" @default.
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