Experimental investigation of multi-step stress-relaxation-ageing of 7050 aluminium alloy for different pre-strained conditions

Author:

Zheng Jing-Hua,Pan Ran,Li Chen,Zhang Wei,Lin Jianguo,Davies Catrin M.

Funder

The Aviation Industry Corporation of China (AVIC) the First Aircraft Institute

International Science & Technology Cooperation Program of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference40 articles.

1. Experimental studies and constitutive modelling of the hardening of aluminium alloy 7055 under creep age forming conditions;Zhan;Int. J. Mech. Sci.,2011

2. Aluminium alloy development for the airbus A380 – part 1;Ph;Adv. Mater. Process.,2007

3. An integrated model to predict residual stress reduction by multiple cold forging operations in extra-large AA7050 T-section panels;Pan;J. Eng. Manuf.,2016

4. Measurement and prediction of machining induced redistribution of residual stress in the aluminium alloy 7449;Robinson;Exp. Mech.,2011

5. A yield strength model for the Al-Mg-Si-Cu alloy AA6111;Esmaeili;Acta Mater.,2003

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