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Microstructure and electrochemical corrosion behavior of selective laser melted Ti−6Al−4V alloy in simulated artificial saliva 被引量:12
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作者 Jiang JU Jing-jing LI +6 位作者 Min JIANG Meng-ya LI Li-xiang YANG Kai-ming WANG Chao YANG Mao-dong KANG Jun WANG 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2021年第1期167-177,共11页
Ti−6Al−4V alloy was fabricated via selective laser melting(SLM)to improve its corrosion resistance for implant.The microstructure and electrochemical corrosion behavior were investigated using scanning electron micros... Ti−6Al−4V alloy was fabricated via selective laser melting(SLM)to improve its corrosion resistance for implant.The microstructure and electrochemical corrosion behavior were investigated using scanning electron microscopy(SEM),electron backscatter diffraction(EBSD),transmission electron microscopy(TEM),electrochemical test and contact angle test.It can be found that the as-selective laser melted(as-SLMed)Ti−6Al−4V alloys showβcolumnar microstructure in building direction and nearly circular checkerboard microstructure in scanning direction,while the wrought and wrought+HT samples exhibit equiaxed microstructure.The as-SLMed Ti−6Al−4V alloy exhibits better corrosion resistance than the wrought and wrought+HT samples due to hydrophobicity,high grain boundary density and uniform distribution of alloying elements in simulated artificial saliva at 37℃. 展开更多
关键词 Ti−6Al−4V alloy selective laser melting MICROSTRUCTURE electrochemical corrosion behavior
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Compression behavior and constitutive model establishment of fly ash cenosphere/polyurethane aluminum alloy syntactic foam 被引量:2
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作者 XU Peng WANG Yonghuan 《Journal of Measurement Science and Instrumentation》 CAS CSCD 2021年第3期369-378,共10页
The aluminum matrix syntactic foam was fabricated by pressure infiltration technique,and the filling material is syntactic foam material with fly ash cenosphere as the main component and polyurethane foam as the binde... The aluminum matrix syntactic foam was fabricated by pressure infiltration technique,and the filling material is syntactic foam material with fly ash cenosphere as the main component and polyurethane foam as the binder.Split Hopkinson pressure bar(SHPB)dynamic compression and quasi-static tests were carried out to examine the compressive response of syntactic foam in this study.Then the dynamic constitutive model was established.Results show that the compressive stress-strain curve of syntactic aluminum foam is similar to that of other metallic foam materials:both kinds of aluminum matrix syntactic foams have strain rate effect,and the syntactic foam has higher compressive strength and energy absorption than the same density aluminum foams.However,due to the different sizes of cenospheres,the dynamic compression results of two kinds of syntactic foams are different,and the energy absorption effect of syntactic foam with small size under dynamic impact is the best.In the range of strain rate and density studied experimentally,the curves of constitutive model fit well with the curves of experimental data. 展开更多
关键词 fly ash cenosphere POLYURETHANE composite foam aluminum strain rate effect mechanical property constitutive model
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轨道再入飞行器气动热力学环境研究 被引量:2
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作者 李翔 王保国 《科技导报》 CAS CSCD 北大核心 2010年第9期73-75,共3页
高超声速飞行器气动热力学环境研究是直接涉及轨道飞行器飞行控制、热防护设计和热安全的关键问题之一。本文借助于多组分、考虑非平衡态气体的振动以及激波与热化学非平衡态效应的守恒积分型Navier-Stokes方程组,使用高分辨率总变差减... 高超声速飞行器气动热力学环境研究是直接涉及轨道飞行器飞行控制、热防护设计和热安全的关键问题之一。本文借助于多组分、考虑非平衡态气体的振动以及激波与热化学非平衡态效应的守恒积分型Navier-Stokes方程组,使用高分辨率总变差减小格式,计算研究了轨道再入飞行器再入地球大气层的10个飞行工况(飞行马赫数9.7~27.8),分析了不同工况下轨道再入飞行器弓形脱体激波后流场气动热力学环境特性,得出气动力系数和沿壁面的热流密度分布,与国外相关飞行数据比较,两者吻合较好。 展开更多
关键词 高超声速 气动热力学 轨道再入飞行器
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