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Experimental Study on Supersonic Combustion Characteristics of Al/B-Kerosene Nanofuels 期刊论文
AIAA JOURNAL, 2024, 页码: 9
Authors:  Fan WH(范文慧);  Zhong FQ(仲峰泉);  Gao ZB(高占彪)
Favorite  |  View/Download：16/0  |  Submit date：2024/05/21
Plasma Assisted Combustion  Petroleum  Nanomaterials  Supersonic Combustor  Flow Measurement  Optical Properties  Boundary Layers  Hydrocarbon Fuels  Band Pass Filter  Heat and Mass Transfer  
Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:  Dai, Chunliang;  Sun, Bo;  Yue LJ(岳连捷);  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yu, Jianyi
Adobe PDF(5674Kb)  |  Favorite  |  View/Download：63/9  |  Submit date：2024/02/19
Scramjet inlet  Starting ability  Thermochemical  Work performance  
Development of interference-free rotational and vibrational thermometry for studies on shock-heated thermochemical non-equilibrium CO 期刊论文
MEASUREMENT SCIENCE AND TECHNOLOGY, 2023, 卷号: 34, 期号: 12, 页码: 14
Authors:  He, Dong;  Si, Ting;  Li F(李飞);  Luo XS(罗喜胜)
Adobe PDF(4040Kb)  |  Favorite  |  View/Download：111/4  |  Submit date：2023/10/30
rotational temperature  vibrational temperature  shock tube  TDLAS  CO  
Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet 期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 193, 页码: 237-254
Authors:  Dai, Chunliang;  Sun, Bo;  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yue LJ(岳连捷)
Adobe PDF(13791Kb)  |  Favorite  |  View/Download：182/42  |  Submit date：2022/05/17
Mach 12 scramjet inlet  High temperature  Non-equilibrium effects  Thermochemical  Inlet performance  
Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 31, 页码: 15683-15696
Authors:  Xue R(薛瑞);  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
Adobe PDF(3251Kb)  |  Favorite  |  View/Download：366/113  |  Submit date：2020/07/06
Compressible boundary layer combustion  Skin-friction reduction  Shock train/flame interaction