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Design of Base Flow for Streamline-Traced Hypersonic Inlet 会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, International Space Planes and Hypersonic Systems and Technologies Conferences, Bremen, Germany, 19 October 2009 - 22 October 2009
Authors:  Yue LJ(岳连捷);  Xiao YB;  Chen LH(陈立红);  Chang XY(张新宇)
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高超声速推进热结构轻量化设计与安全评估 会议论文
第一届高超声速科技学术会议, 云南·丽江, 2008-12-28
Authors:  宋宏伟;  黄晨光;  范学军;  仲峰泉
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用于发动机热防护材料烧蚀实验的小型等离子体风洞 会议论文
第一届高超声速科技学术会议, 云南·丽江, 2008-12-28
Authors:  黄河激;  潘文霞;  付志强;  吴承康
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双路喷注超临界态煤油的超燃特性研究 会议论文
第一届高超声速科技学术会议, 云南丽江, 2008
Authors:  范学军;  仲峰泉;  王晶;  俞刚;  李建国
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超临界压力下航空煤油热裂解特性研究 会议论文
第一届高超声速科技学术会议, 云南丽江, 2008
Authors:  仲峰泉;  范学军;  王晶
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Investigation on a truncated streamline-traced hypersonic Busemann inlet 会议论文
15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, United states, April 28, 2008 - May 1, 2008
Authors:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Gong P;  Chang XY(张新宇)
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Boundary Layer Corrections  Busemann Inlet  Core Flow  Correction Method  Design Points  Finite Differential Methods  Internal Contraction Ratio  Internal Flows  Mass Flow  
斜爆轰与斜爆轰推进系统的研究进展 会议论文
第十三届全国激波与激波管学术会议, 湖南长沙, 2008-05
Authors:  王爱峰;  赵伟
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斜爆轰  斜爆轰推进  冲压加速器  
Research progress on high-enthalpy and hypersonic flows 会议论文
5th International Conference on Fluid Mechanics, Shanghai, PEOPLES R CHINA, AUG 15-19, 2007
Authors:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒);  Lin ZB(林贞彬);  Jiang Z
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Hypersonic Flows  Detonation Driver  Shock-reflected Tunnels  Shock-expanded Tube  Heat Transfer  
双翼振动的预处理数值方法和性能研究(二) 会议论文
第九届全国振动理论及应用学术会议暨中国振动工程学会成立20周年庆祝大会, 浙江杭州, 2007
Authors:  王涛;  刘鹏飞;  杨国伟
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Performance of supersonic model combustors with distributed injection of supercritical kerosene 会议论文
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cincinnati, OH, United states, July 8, 2007 - July 11, 2007
Authors:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Lu XN;  Sung CJ
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Stagnation Temperatures  Supercritical Kerosene  Supersonic Model Combustors