Peng Jin

Dr. Peng Jin


Research Focus & Metrics

Academic Career Length

15Years (2012-Present)

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

Representative Publications

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28 May 2020 in Structural and Multidisciplinary Optimization
Verified
Journal Article
Closed access
PDF file
QZQi Zhou
Qi Zhou
YWYuda Wu
Yuda Wu
ZGZhendong Guo
Zhendong Guo
JHJiexiang Hu
Jiexiang Hu
PJPeng Jin
Peng Jin

20 August 2019 in Engineering with Computers
Verified
Journal Article
Closed access
PDF file
QZQi Zhou
Qi Zhou
JWJinhong Wu
Jinhong Wu
TXTao Xue
Tao Xue
PJPeng Jin
Peng Jin

2 November 2024 in Construction and Building Materials
Verified
Journal Article
Closed access
PJPeng Jin
Peng Jin
LLLi Li
Li Li
ZLZongli Li
Zongli Li
WDWeiyi Du
Weiyi Du
Mehran KhanMehran Khan
Mehran Khan
ZLZongjin Li
Zongjin Li

23 September 2020 in Journal of Intelligent Manufacturing
Verified
Journal Article
Closed access
PDF file
JLJingchang Li
Jingchang Li
LCLongchao Cao
Longchao Cao
JHJiexiang Hu
Jiexiang Hu
MSMinhua Sheng
Minhua Sheng
QZQi Zhou
Qi Zhou
PJPeng Jin
Peng Jin

4 April 2023 in Mechanics of Advanced Materials and Structures
Verified
Journal Article
Closed access
BLBowen Li
Bowen Li
FZFeng Zhang
Feng Zhang
PJPeng Jin
Peng Jin
This paper proposed a composite sandwich structure containing multilayer honeycombs, and a multi-objective optimization model containing its load-bearing and wave-absorbing properties, which were correlated with the geometric parameters of the honeycomb, was developed. The critical elastic buckling load was performed as an indicator to characterize the load-bearing capacity, and the bandwidth of the sandwich was employed as an indicator to characterize the wave-absorbing characteristics. This multi-objective optimization model was optimized based on JAYA algorithm and the results showed that the optimized structure had a significant improvement in both load-bearing and wave-absorbing capacities compared to the original structure.

1 April 2016 in The Aeronautical Journal
Verified
Journal Article
Closed access
PDF file
PJPeng Jin
Peng Jin
XZX. Zhong
X. Zhong
JYJ. Yang
J. Yang
ZSZ. Sun
Z. Sun
In this paper, a new optimisation method incorporating lamination parameters and a guide-based blending model is proposed. Lamination parameters for a guide laminate and ply number of each panel are employed as design variables for optimisation with a parallel real-coded genetic algorithm incorporating structure behaviour and manufacturing constraints. During the optimisation process, with a form of least squares fitting adopted, another genetic algorithm is used to obtain the guide stacking sequence of the guide laminate from the guide lamination parameters, and then the laminate configurations of each panel are obtained from the guide stacking sequence and number of plies for each panel. The proposed framework is demonstrated via design of an 18-panel horseshoe configuration, where each panel is optimised individually with a buckling constraint. Numerical results indicate that the present algorithm is capable of obtaining fully blended designs.