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Experimental investigation of mode transition process in a cavity-based scramjet 期刊论文
PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 4, 页码: 11
Authors:  Meng Y(孟宇);  Sun WM(孙文明);  Gu HB(顾洪斌);  Chen, Fang
Favorite  |  View/Download：24/0  |  Submit date：2024/05/14
Large Eddy Simulation of Axisymmetric Scramjet Based on Dynamic Zone Flamelet Model 会议论文
Asia-Pacific International Symposium on Aerospace Technology (APISAT), Korean Soc Aeronaut & Space Sci, Jeju, SOUTH KOREA, NOV 15-17, 2021
Authors:  Sun WM(孙文明);  Liu H(刘杭);  Li L(李龙);  Yao W(姚卫)
Adobe PDF(2371Kb)  |  Favorite  |  View/Download：206/53  |  Submit date：2022/11/24
Axisymmetric scramjet  Ethylene  Improved Delay Detached Eddy Simulation (IDDES)  Dynamic Zone Flamelet Model (DZFM)  Cavity  
Supersonic Combustion Mode Analysis of a Cavity Based Scramjet 期刊论文
AEROSPACE, 2022, 卷号: 9, 期号: 12, 页码: 826
Authors:  Meng, Yu;  Sun WM(孙文明);  Gu HB(顾洪斌);  Chen, Fang;  Zhou RX(周芮旭)
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scramjet  combustion mode  POD  instability  
微波对超声速燃烧影响实验研究 学位论文
硕士论文，北京: 中国科学院大学, 2020
Authors:  孙文明
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微波  超声速燃烧  火焰速度  火焰位置  火焰稳定性  
微波增强滑移电弧等离子体辅助超声速燃烧 期刊论文
航空学报, 2020, 卷号: 41, 期号: 2, 页码: 123345
Authors:  孟宇;  顾洪斌;  孙文明;  张新宇
View  |  Adobe PDF(945Kb)  |  Favorite  |  View/Download：259/38  |  Submit date：2019/12/16
超燃冲压发动机  超声速燃烧  等离子体助燃  滑移电弧  微波  
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：381/100  |  Submit date：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration  
一种用于超燃冲压发动机的微波天线模块 专利
发明专利. 一种用于超燃冲压发动机的微波天线模块, 专利号: ZL201811375118.7, 申请日期: 2018-11-19,
Inventors:  孟宇;  顾洪斌;  孙文明
View  |  Adobe PDF(393Kb)  |  Favorite  |  View/Download：176/34  |  Submit date：2020/02/10