YuFeng Xia

Prof. YuFeng Xia


Research Focus & Metrics

Academic Career Length

4Years (2023-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 March 2024 in Journal of Central South University
Verified
Journal Article
Closed access
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DZDe-Yu Zheng
De-Yu Zheng
YXYuFeng Xia
YuFeng Xia
HTHai-Hao Teng
Hai-Hao Teng
YYYingyan Yu
Yingyan Yu

19 May 2023 in Metals
Verified
Journal Article
Open access
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HTHai hao Teng
Hai hao Teng
YXYuFeng Xia
YuFeng Xia
CPChenghai Pan
Chenghai Pan
YLYan Li
Yan Li
The 7050 alloy is a kind of Al-Zn-Mg-Cu alloy that is widely used for aircraft structures. Although the deformation behavior of the solid solution state 7050 aluminum alloy is critical for engineering and manufacturing design, it has received little attention. In this study, the room and warm compression behavior of the solid solution-state 7050 alloy was researched, and a modified model with variable parameters was built for the flow stress and load prediction. The isothermal compression tests of the solid solution-state 7050 alloy were performed under the conditions of a deformation temperature of 333–523 K, a strain rate of 10−3–10−1 s−1, and a total reduction of 50%. The strain-stress curves at different temperatures were corrected by considering interface friction. The flow stress model of aluminum was established using the modified Voce model. For evaluating the modified Voce model’s prediction accuracy, the flow stresses calculated by the model were compared with the experimental values. Consequently, for assessing its prediction abilities in finite element applications, the whole compression process was simulated in the finite element analysis platform. The results sufficiently illustrated that the modified Voce-type model can precisely predict the complex flow behaviors during warm compression. This study will guide the prediction of the warm compression load and the optimization of the heat treatment process of the alloy.

1 October 2025 in Journal of Central South University
Verified
Journal Article
Closed access
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YXYuFeng Xia
YuFeng Xia
XDXiao Du
Xiao Du
FSFen Sun
Fen Sun
DZDe-Yu Zheng
De-Yu Zheng
HZHao-Nan Zou
Hao-Nan Zou
WYWen-Bin Yang
Wen-Bin Yang

10 March 2023 in Materials
Verified
Journal Article
Open access
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YXYuFeng Xia
YuFeng Xia
WYWenbin Yang
Wenbin Yang
YYYingyan Yu
Yingyan Yu
HTHai hao Teng
Hai hao Teng
QCQian Cheng
Qian Cheng
The plastic deformation behavior of a CHN327 nickel-based superalloy under temperatures ranging from 600 °C to 700 °C and strain rates ranging from 0.001 to 0.1 s−1 was investigated using uniaxial high-temperature tensile tests. The stress–strain curves obtained by the tests showed that the maximum stress decreased as the temperature increased, while it increased as the strain rate increased. Based on the extensive data obtained in the experiment, three constitutive models (Hollomon, Swift, and the modified Voce equation) were employed to predict the constitutive relation. It was found that the modified Voce equation had the highest correlation coefficient and the best prediction accuracy. Thereafter, in order to predict the fracture of CHN327 during high-temperature tensile deformation, five ductile fracture criteria (Freudenthal, C&L, Brozzo, Ayada, and the R&T model), and the modified Voce equation obtained were incorporated into the finite element software (DEFORM). According to the results, except for the C&L and Brozzo models, all of the other ductile fracture criteria (DFCs) were suitable for predicting the damage distribution of the CHN327 alloy in tensile tests. For all of the DFCs considered, the R&T model provided the most accurate predictions, whose mean error was only 8.9%, far less than the values that other models predicted.

24 October 2024 in Journal of Materials Engineering and Performance
Verified
Journal Article
Closed access
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HTHaihao Teng
Haihao Teng
YXYuFeng Xia
YuFeng Xia
YYYingyan Yu
Yingyan Yu
TSTao Sun
Tao Sun

23 October 2025 in Journal of Materials Engineering and Performance
Verified
Journal Article
Closed access
PDF file
HTHai-Hao Teng
Hai-Hao Teng
YXYuFeng Xia
YuFeng Xia