Mathematical Modeling of the Heat Treatment Processes Applied to Alloy Al-Zn-Mg-Cu-4.5% Zn Used in Aeronautics
Keywords:
mathematical modeling, aluminum alloy, heat treatment
Abstract
This paper presents mathematical modeling based on the regression analysis method by active experiment of a thermal treatment process applied to an alloy belonging to Al-Zn system, which finds application in aeronautics.
Using the mathematical model determined on a statistical basis, we achieved the prediction of the mechanical properties studied by simulating the heat treatment process, more exactly by simulating the heat treatment parameter values within the experimental values.
The mathematical model equations obtained in this paper can also be used to achieve the optimal values of the treatment technological parameters in order to obtain the desired complex of properties with minimum costs.
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References
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[2]. Baron, T. s.a. - Statistică teoretică şi economică. Editura Didactică şi Pedagogică, Bucureşti, (1995).
[3]. Naisnith, S.J. - Encyclopedia dictionary of mathematics for engineers and applied scientists. Editura S.J.N, Oxford, (1986).
[4]. Nistor, L. ş. a. - Modelarea formei secţiunii transversale a laminatului prin optimizarea puterii consumate în procesul de laminare pe principiul metodei de calcul variaţional. În rev. Metalurgia nr. 5, (1995).
[5]. A. Brăgaru, C. Picoş, N. Ivan – Optimizarea proceselor şi echipamentelor tehnologice, Editura didactică şi pedagogică, Bucureşti, (1996).
Published
2012-12-15
How to Cite
1.
NEACSU M, HANGANU D. Mathematical Modeling of the Heat Treatment Processes Applied to Alloy Al-Zn-Mg-Cu-4.5% Zn Used in Aeronautics. The Annals of “Dunarea de Jos” University of Galati. Fascicle IX, Metallurgy and Materials Science [Internet]. 15Dec.2012 [cited 24Nov.2024];35(4):73-7. Available from: https://gup.ugal.ro/ugaljournals/index.php/mms/article/view/2870
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