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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
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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
View  |  Adobe PDF(3156Kb)  |  Favorite  |  View/Download:20/3  |  Submit date:2020/01/08
总焓  电弧加热器  氧原子  发射光谱  漏水诊断  
Numerical study of wedge-induced oblique detonations in unsteady flow 期刊论文
JOURNAL OF FLUID MECHANICS, 2019, 卷号: 876, 页码: 264-287
Authors:  Yang PF(杨鹏飞);  Ng HD;  Teng HH(滕宏辉)
View  |  Adobe PDF(1356Kb)  |  Favorite  |  View/Download:69/5  |  Submit date:2019/09/09
detonations  
Statistical analysis of temperature distribution on vortex surfaces in hypersonic turbulent boundary layer 期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 10, 页码: 7
Authors:  Lin X(林鑫);  Tong FL(童福林);  Yu ZP(于长平);  Li XL(李新亮)
Favorite  |  View/Download:2/0  |  Submit date:2020/03/11
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)
View  |  Adobe PDF(3099Kb)  |  Favorite  |  View/Download:50/11  |  Submit date:2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration  
JF12激波风洞高Mach数超燃冲压发动机实验研究 期刊论文
气体物理, 2019, 卷号: 4, 期号: 05, 页码: 25-31
Authors:  姚轩宇;  王春;  喻江;  苑朝凯;  姜宗林;  司徒明
View  |  Adobe PDF(2036Kb)  |  Favorite  |  View/Download:53/11  |  Submit date:2020/01/08
超燃冲压发动机  高Mach数  激波风洞  纯净空气  JF12风洞  
Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor 期刊论文
JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 32, 期号: 5, 页码: 11
Authors:  Cheng D(程迪);  Wang J(王晶);  Lu Y(陆阳);  Li L(李龙);  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(2651Kb)  |  Favorite  |  View/Download:65/11  |  Submit date:2019/09/09
Heat flux measurement  Kerosene  Supersonic combustion  Scramjet  Heat flux sensor  
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
Favorite  |  View/Download:2/0  |  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
View  |  Adobe PDF(663Kb)  |  Favorite  |  View/Download:64/3  |  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  
双楔面诱导斜爆轰波起爆特性研究 会议论文
中国力学大会, 中国浙江杭州, 2019年8月25-28日
Authors:  张宇航;  杨鹏飞;  滕宏辉
View  |  Adobe PDF(1847Kb)  |  Favorite  |  View/Download:19/4  |  Submit date:2019/11/21
斜爆轰波  两步反应  激波相互作用  诱导机制  起爆长度