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14篇 您的检索式:作者名="Bangming Tang"
    题名 作者 年代 出处 被引量
1Toughness improvement of carbon laminates by periodic interleaving thin thermoplastic films显示文摘A. N. Xuefeng J. I. Shuangying Tang Bangming Zhang Zilong Yi Xiao-Su 2002Journal of Materials Science Letters2002,,22:1
2Ex- situ formation of periodic interlayer structure to improve significantly the impact damage resistance of carbon laminates 显示文摘Yi Xiaosu An Xuefeng Tang Bangming 2003Advanced Engineering Materials2003,5,10:1
3Toughness improvement of carbon laminates by periodic interleaving thin thermoplastic films 显示文摘An Xuefeng Ji Shuangying Tang Bangming 2002Journal of Material Science Letters2002,21,:1
4Toughness improvement of carbon laminates by periodic interleaving thin films 显示文摘An Xuefeng Tang Bangming Yi Xiaosu 2002Journal of Materials Science Letters2002,21,22:1
5Ex- situ formation of periodic interlayer structure to imptove significantly the impact damage resistance of carbon laminates 显示文摘Yi Xiaosu An Xuefeng Tang Bangming 2003Advance Engineering Materials2003,5,10:1
6Ex-situ concept for toughening the RTMable BMI matrix composites I: Improving the interlaminar fracture toughness 显示文摘Cheng Qunfeng Fartg Zhengping Yi Xiaosu An Xuefeng Tang Bangming Xu Yahong 2008Journal of Applied Polymer Science2008,109,3:1
7Ex-situ concept for toughening the RTMable BMI matrix composites Ⅱ Improving the compression after impact 显示文摘Cheng Qunfeng Fang Zhengping Yi Xiaosu An Xuefeng Tang Bangming Xu Yahong 2008Journal of Applied Polymer Science2008,108,4:1
8Toughness improvement of carbon laminates by periodic interleaving thin films显示文摘An Xuefeng Tang Bangming Yi Xiaosu 2002Journal of Materials Science Letters2002,21,22:1
9“Ex situ” concept for toughening the RTMable BMI matrix composites Part I ; Improving the interlaminar fracture toughness显示文摘Cheng Qunfeng Fang Zhengping Yi Xiaosu An Xuefeng Bangming Tang Yahong Xi 2008Journal of Applied Polymer Science2008,109,3:1
10Ex-situ Formation Periodic Interlayer Structure to Improve Significantly the Impact Damage Resistance of Carbon Laminates 显示文摘Yi Xiaosu An Xuefeng Tang Bangming 2003Advanced Engineering materials2003,5,0:1
11Ex-Situ Formation of Periodic Interlayer Structure to Improve Significantly the Impact Damage Resistance of Carbon Laminates 显示文摘Yi Xiaosu An Xuefeng Tang Bangming 2003Advanced Engineering Materials2003,5,10:1
12Toughness Improvement of Carbon Laminates by Periodic Interleaving Thin Thermoplastic Films 显示文摘An Xuefeng Ji Shuangying Tang Bangming 2002Journal of Material Science Letters2002,21,:1
13TTT Diagram and Phase Structure Control of 2/4 Functional Epoxy Blends Used in Advanced Composites显示文摘Zhang Ming An Xuefeng Tang Bangming 2007Frontiers of Materials Science in China2007,1,1:1
14TTT Diagram Used to Control Phase Structure of 2/4 Functional Epoxy Blends for Advanced Composites显示文摘This article uses a 2/4 functional epoxy blend system(E-54/AG-80) cured with diaminodiphenyl sulphone(DDS) as a raw material and develops a methodological procedure to establish a cure kinetic model with isothermal and dynamic differential scanning calorimeter(DSC) method and a gelation model with round-disk compression mode dynamic mechanical analyzer(DMA),thus acquiring a series of experimental data.Characteristic temperatures such as initial glass transition temperature Tg0,gelation glass transition temperature gelTg,and infinite glass transition temperature Tg∞ are determined.The cure degree at gelation is turned out to be 0.45,while gelTg is found to be 70.2 °C.The data are then used to form time-temperature-transition(TTT) diagram of the system,which serves to be a tool for process optimization of epoxy-matrix composites.A new cure processing is therefore derived from the TTT diagram.The final phase structure obtained from a controllable method is identified through scanning electron microscope(SEM) photographs to be of 'ex-situ' phase morphology.Zhang Ming,An Xuefeng,Tang Bangming,Yi Xiaosu National Key Laboratory of Advanced Composites Materials,Beijing Institute of Aeronautical Materials,Beijing,100095,China 2009Chinese Journal of Aeronautics2009,22,4:0
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