According to the curing process of composite laminate, a simplified one-dimensional (1D) transient heat conduction model for the composite laminate is established. Based on a typical curing technological curve, the relationships are studied among the processing conditions including convective heat transfer coefficient, the thickness of the part, Fourier number and surplus temperature etc. Furthermore, the useful engineering charts for the center surplus temperature of the composite laminate in the thickness direction are given. Also based on the simplified 1D model, temperature field for the three-dimensional (3D) laminate structure under the hold stage which lay on top of a conforming mold is determined. Then based on the temperature field, the internal strain and curvature distribution of the curing composite laminate are calculated.
Kong Kwong, Wah Hospital, Xiangyu Zou, Yong Zhang, Yang Liu, Lei Shi, D Kan, Wu Ouyang, L Chen, S Liu, Da Chen, Yifei Ma, Chengqiang Cui, Qiang Zhang, W Lao, Chunlin Huang, Heng Ban, Hai Lu, Yan Shi, Qi Si, Yan Ding, Zong Li, Haozhe Liu, Zengwu Shao, Yulong Li, Siwei Song, Jin Wang, Yang Liu, H Dong, X Liu High, Wang We, A Sharhan, Ershun Du, Xinyu Hu, Zhenhuan Zhou, Jian Lü, Yankun Tang, A Abdelrahman, M Ghannam, S Lotfy, Mohammad AlHamaydeh, Xiang Xiong, F Nkuichou, Tao Wang, M Ma, K Du Corrosion, Na Wang, Jianmin Hua, Xin Xue, Qiao Huang, Fei Wang, Haibo Huang, Liang Ren, Kun Chen, X Li, Lei Wang, Bing Yang, Mingming Zhang, Wenjun Liu, Z Lei, Dongying Wang, Jiabin Wang, Li Zhou, Xueming Shu, Cross-Sections Zhang, Leroy Gardner, C Buchanan, Dave Chan, Wei Sun, Yu Wang, Qing He, Ran Li, Cong Xue, Tao Lan, Guangzhao Qin
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