An inverse strategy to determine constitutive parameters of tubular materials for hydroforming processes

Bin ZHANG*, Benny ENDELT, Lihui LANG, Yang ZHAO, Shu YAN, Karl Brian NIELSEN

*Kontaktforfatter

Publikation: Bidrag til tidsskriftTidsskriftartikelForskningpeer review

3 Citationer (Scopus)
30 Downloads (Pure)

Abstract

This paper is to determine the flow stress curve of 5049-O aluminium alloy by a tube hydraulic bulging test with fixed end-conditions. During this test, several tubular specimens are bulged under different internal pressures before their bursting, and the corresponding bulging height and wall thickness at the pole are measured. An inverse strategy is developed to determine the constitutive parameters of tubular materials based on experimental data, which combines the finite element method with gradient-based optimization techniques. In this scheme, the objective function is formulated with the sum of least squares of the error between numerical and experimental data, and finite difference approximation is used to calculate the gradient. The tubular material behavior is assumed to meet the von Mises yield criterion and Hollomon exponential hardening law. Then, constitutive parameters identification is performed by minimization of the objective function. In order to validate the performance of this framework, identified parameters are compared with those obtained by two types of theoretical models, and tensile tests are performed on specimens cut from the same tubes. The comparison shows that this inverse framework is robust and can achieve a more accurate parameter identification by eliminating mechanical and geometrical assumptions in classical theoretical analysis.

OriginalsprogEngelsk
TidsskriftChinese Journal of Aeronautics
Vol/bind35
Udgave nummer6
Sider (fra-til)379-390
Antal sider12
ISSN1000-9361
DOI
StatusUdgivet - jun. 2022

Bibliografisk note

Funding Information:
The first author acknowledges the financial support from China Scholarship Council (CSC) (No. 201706080020) for his study at Aalborg University in Denmark.

Publisher Copyright:
© 2021 Chinese Society of Aeronautics and Astronautics

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