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高超声速飞行器新型热防护机制研究进展 被引量:27
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作者 梁伟 金华 +3 位作者 孟松鹤 杨强 曾庆轩 许承海 《宇航学报》 EI CAS CSCD 北大核心 2021年第4期409-424,共16页
从气动热载荷的来源出发,介绍了基于流动控制、光辐射操控、原子重组、电子耗散等物理机制的新型热防护机制的原理和进展。分别从环境和材料两方面实现对流热、化学热和辐射热的主动调控,进一步分析了高超声速飞行器新型热防护机制发展... 从气动热载荷的来源出发,介绍了基于流动控制、光辐射操控、原子重组、电子耗散等物理机制的新型热防护机制的原理和进展。分别从环境和材料两方面实现对流热、化学热和辐射热的主动调控,进一步分析了高超声速飞行器新型热防护机制发展的特点和不足,对该领域未来研究的重点方向提出了建议。 展开更多
关键词 高超声速飞行器 热防护机制 对流热 化学热 辐射热
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Mechanical properties of 3D carbon/carbon composites by nanoindentation technique 被引量:5
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作者 WEI Li-ming ZHANG Yue +2 位作者 XU Cheng-hai QI Fei meng song-he 《Journal of Central South University》 SCIE EI CAS 2012年第1期36-40,共5页
Nanoindentation tests were conducted to investigate the near-surface mechanical properties of the individual components(fiber and matrix) for three-dimensional reinforced carbon/carbon composites(3D C/C).Optical micro... Nanoindentation tests were conducted to investigate the near-surface mechanical properties of the individual components(fiber and matrix) for three-dimensional reinforced carbon/carbon composites(3D C/C).Optical microscope and polarizing light microscope were used to characterize the microstructure of 3D C/C.The microscopy results show that large number of pores and cracks exist at both bundle/matrix interface and pitch carbon matrix.These defects have important effect on the mechanical behavior of 3D C/C.The in situ properties for components of 3D C/C were acquired by nanoindentation technique.Relative to the matrix sample,the fiber samples have more larger values for modulus,stiffness and hardness.However,there is no significant difference of modulus and stiffness among fiber samples with different directions. 展开更多
关键词 C/C composites mechanical properties NANOINDENTATION MICROSTRUCTURE
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Fabrication and thermo-physical properties of TiB_(2p)/Cu composites for electronic packaging applications
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作者 CHEN Guo-qin XIU Zi-yang +2 位作者 meng song-he WU Gao-hui ZHU De-zhi 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2009年第S02期448-452,共5页
TiB_(2p)/Cu composites with high reinforcement content(φ_(p)=50%,58%and 65%)for electronic packaging applications were fabricated by squeeze casting technology.The microstructures and thermo-physical properties of th... TiB_(2p)/Cu composites with high reinforcement content(φ_(p)=50%,58%and 65%)for electronic packaging applications were fabricated by squeeze casting technology.The microstructures and thermo-physical properties of the TiB_(2p)/Cu composites were investigated.The results show that TiB2 particles are homogeneous and distribute uniformly,and the TiB2-Cu interfaces are clean and free-from interfacial reaction products and amorphous layers,the densifications of the TiB_(2p)/Cu composites are higher than 98.2%. The mean linear coefficients of thermal expansion at 20-100℃for TiB_(2p)/Cu composites range from 8.3×10^(-6)to 10.8×10^(-6)/K and decrease with increasing volume fraction of TiB2.The experimental coefficients of thermal expansion agree well with the predicted values based on Turner’s model.The thermal conductivities of TiB_(2p)/Cu composites range from 167.3 to 215.4 W/(m·K),decreasing with increasing volume fraction TiB2. 展开更多
关键词 TiB_(2p)/Cu composites DENSIFICATION coefficient of thermal expansion thermal conductivity
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