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Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 171, 页码: 300-310
Authors:  Ju SJ;  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
Favorite  |  View/Download:30/0  |  Submit date:2020/05/18
Computational fluid dynamics  Drag reduction  Supersonic flow  Energy deposition  Opposing jet  
Comparison of Strategies for Coupled Flow-Thermal Analysis of Thermal Protection System at Hypersonic Flight Condition 期刊论文
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 卷号: 21, 期号: 2, 页码: 347-362
Authors:  Wang RX(王睿星);  Wang, ZW;  Zheng HW(郑洪伟);  Song HW(宋宏伟)
Favorite  |  View/Download:19/0  |  Submit date:2020/06/22
Coupled flow-thermal analysis  Thermal protection system  Basic direct correction method (BDCM)  Improved DCM (IDCM)  Iteration solution method (ISM)  
超燃冲压发动机加速过程及等离子体对超声速火焰结构的影响 学位论文
博士论文,北京: 中国科学院大学, 2019
Authors:  孟宇
Adobe PDF(11443Kb)  |  Favorite  |  View/Download:184/9  |  Submit date:2019/11/07
超燃冲压发动机,燃烧模态,火焰结构,加速过程,微波,滑移电弧,等离子体  
基于原子发射光谱的中低焓电弧加热器漏水故障诊断 期刊论文
实验流体力学, 2019, 卷号: 33, 期号: 05, 页码: 82-87
Authors:  林鑫;  曾徽;  彭锦龙;  欧东斌;  李飞;  余西龙
Adobe PDF(3156Kb)  |  Favorite  |  View/Download:37/8  |  Submit date:2020/01/08
总焓  电弧加热器  氧原子  发射光谱  漏水诊断  
Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316
Authors:  Meng Y(孟宇);  Gu HB(顾洪斌);  Zhuang JH(庄金衡);  Sun WM(孙文明);  Gao ZB(高占彪);  Lian H(连欢);  Yue LJ(岳连捷);  Chang XY(张新宇)
Adobe PDF(3099Kb)  |  Favorite  |  View/Download:73/18  |  Submit date:2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration  
Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108
Authors:  Zhu JJ;  Wang XJ;  Zhang HG;  Li YW;  Wang RX(王睿星);  Qiu ZP
Adobe PDF(2082Kb)  |  Favorite  |  View/Download:14/0  |  Submit date:2020/03/21
Hypersonic vehicle  Six sigma robust optimization  Successive response surface  Thermal protection system  Uncertainty  
设计参数对幂次乘波体纵向静稳定性的影响 期刊论文
宇航学报, 2019, 期号: 08, 页码: 887-896
Authors:  王晓朋;  张陈安;  刘文;  王发民;  叶正寅
Adobe PDF(663Kb)  |  Favorite  |  View/Download:93/6  |  Submit date:2019/09/12
纵向静稳定性  幂次乘波体  高超声速滑翔飞行器  
高速双锥绕流中热化学与输运模型影响研究 期刊论文
力学学报, 2019, 卷号: 51, 期号: 04, 页码: 1012-1021
Authors:  丛彬彬;  万田
Adobe PDF(3373Kb)  |  Favorite  |  View/Download:18/0  |  Submit date:2019/09/12
激波边界层相互作用  热化学非平衡  输运模型  双锥  
高超声速高焓风洞试验技术研究进展 期刊论文
空气动力学学报, 2019, 卷号: 37, 期号: 03, 页码: 347-355
Authors:  姜宗林
Adobe PDF(1099Kb)  |  Favorite  |  View/Download:59/9  |  Submit date:2019/09/12
高焓流动  激波风洞  高超声速飞行器  气动力/热特性  测量技术  
The Effects of Combustion on Turbulent Statistics in a Supersonic Turbulent Jet 期刊论文
ADVANCES IN APPLIED MATHEMATICS AND MECHANICS, 2019, 卷号: 11, 期号: 3, 页码: 664-674
Authors:  Fu YW(符耀威);  Yu ZP(于长平);  Yan Z(闫政);  Li XL(李新亮)
Adobe PDF(82Kb)  |  Favorite  |  View/Download:185/8  |  Submit date:2019/04/11
Supersonic jet  turbulent combustion  direct numerical simulation