IMECH-IR

浏览/检索结果: 共8条,第1-8条 帮助

限定条件        
已选(0)清除 条数/页:   排序方式:
Aerodynamic optimization of hypersonic blunted waveriders based on symbolic regression 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 18
作者:  Guo SQ(郭帅旗);  Liu W(刘文);  Zhang CA(张陈安);  Liu Y(刘洋);  Wang FM(王发民)
收藏  |  浏览/下载:25/0  |  提交时间:2024/02/05
Hypersonic waverider  Aerodynamic model  Symbolic regression  Bluntness effect  
Detonation wave structure and thrust variation of a ram accelerator with different projectile velocities 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 143, 页码: 8
作者:  Shang JH(尚甲豪);  Wang, Kuanliang;  Wang, Aifeng;  Wang Q(汪球);  Zhao W(赵伟)
Adobe PDF(4127Kb)  |  收藏  |  浏览/下载:78/6  |  提交时间:2024/01/02
Ram accelerator  Detonation  Oblique detonation wave  Recirculation zone  
Control of shock-wave/boundary-layer interaction using abackward-facing step 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 126, 页码: 13
作者:  Zhai J;  Zhang CA(张陈安);  Wang FM(王发民);  Zhang WW(张伟为)
Adobe PDF(4533Kb)  |  收藏  |  浏览/下载:158/37  |  提交时间:2022/12/20
Shock-wave/boundary-layer interaction  Backward-facing step  Flow separation  Hypersonic inlet  
Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
作者:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(1961Kb)  |  收藏  |  浏览/下载:270/103  |  提交时间:2020/05/18
Hybrid rocket engine  Paraffin-based fuel  Acrylonitrile-butadiene-styrene  Regression rate  Combustion efficiency  
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
作者:  Wang KL(王宽亮);  Li F(李飞);  Zou PF(邹鹏飞);  Lin X(林鑫);  Mao RH(毛荣海);  Yu XL(余西龙)
浏览  |  Adobe PDF(2678Kb)  |  收藏  |  浏览/下载:270/61  |  提交时间:2020/03/21
Swirl flame  Heat release  Chemiluminescence  3D-CTC  
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
作者:  Wang KL(王宽亮);  Li F(李飞);  Zou PF(邹鹏飞);  Lin X(林鑫);  Mao RH(毛荣海);  Yu XL(余西龙)
浏览  |  Adobe PDF(2678Kb)  |  收藏  |  浏览/下载:206/68  |  提交时间:2020/03/21
Swirl flame  Heat release  Chemiluminescence  3D-CTC  
Tunable diode laser absorption spectroscopy measurements of high-pressure ammonium dinitramide combustion 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 45, 页码: 140-149
作者:  Yao, Zhaopu;  Zhang, Wei;  Wang, Meng;  Chen, Jun;  Shen, Yan;  Wei, Yanming;  Yu XL(余西龙);  Li F(李飞);  Ceng H(曾徽);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Unknown(1847Kb)  |  收藏  |  浏览/下载:240/69  |  提交时间:2015/10/21
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
作者:  Wang ZP(王知溥);  Li F(李飞);  Gu HS;  Yu XL(余西龙);  Zhang XY(张新宇);  Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1112Kb)  |  收藏  |  浏览/下载:544/226  |  提交时间:2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas