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Parameters for evaluating the efficiency of inlet compression 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
作者:  Chen KT(陈科挺);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(511Kb)  |  收藏  |  浏览/下载:207/41  |  提交时间:2022/01/12
Airbreathing engine  Compression efficiency  Compression quality  Inlet  Self-consistency  
Combustion Characteristic and Mechanism of a Mixture Working Fluid C3H8/CO2 期刊论文
JOURNAL OF THERMAL SCIENCE, 2021, 页码: 12
作者:  Shi Weixiu;  Pan LS(潘利生);  Jin Suyi;  Dong YH(董跃华);  Li T(李腾);  Zhao J(赵京);  Wei XL(魏小林)
Adobe PDF(2198Kb)  |  收藏  |  浏览/下载:247/54  |  提交时间:2021/11/01
CO2-based mixture  flammability  laminar flame speed  flammable critical mixing ratio  transcritical power cycle  
Experimental Investigation on the Performance of [APMIm][NTf2] for Capturing CO2 from Flue Gas of the Cement Kiln Tail 期刊论文
JOURNAL OF THERMAL SCIENCE, 2021, 页码: 9
作者:  Pan LS(潘利生);  Shi, Weixiu;  Li, Bing;  Wei, Xiaolin
Adobe PDF(1424Kb)  |  收藏  |  浏览/下载:272/59  |  提交时间:2021/09/07
ionic liquid  CO2 absorption  Carbon Capture Utilization and Storage (CCUS)  flue gas of the cement kiln tail  
Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
作者:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
Adobe PDF(1806Kb)  |  收藏  |  浏览/下载:282/56  |  提交时间:2021/05/17
Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
作者:  Yuan CK(苑朝凯);  Jiang ZL(姜宗林)
Adobe PDF(3790Kb)  |  收藏  |  浏览/下载:390/60  |  提交时间:2021/03/03
Hypersonics  Shock tunnels  Flow characteristics  
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
作者:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  收藏  |  浏览/下载:329/170  |  提交时间:2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
作者:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH(马生虎);  Zhang QF(张启帆);  Zhang, Peng;  Zhang XY(张新宇)
Adobe PDF(3937Kb)  |  收藏  |  浏览/下载:196/48  |  提交时间:2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
Numerical investigations of the transient cavitating vortical flow structures over a flexible NACA66 hydrofoil 期刊论文
JOURNAL OF HYDRODYNAMICS, 2020, 卷号: 32, 期号: 5, 页码: 865-878
作者:  Huang RF(黄仁芳);  Du TZ(杜特专);  Wang YW(王一伟);  Huang CG(黄晨光)
Adobe PDF(4739Kb)  |  收藏  |  浏览/下载:319/87  |  提交时间:2020/12/28
Cloud cavitation  LARGE-EDDY SIMULATION  flexible hydrofoil  VORTEX IDENTIFICATION METHODS  Ω  SPECIAL EMPHASIS  method  ADDED-MASS  flow-induced vibration  OMEGA  VIBRATION  DYNAMICS  
Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177
作者:  Yao W(姚卫)
浏览  |  Adobe PDF(9586Kb)  |  收藏  |  浏览/下载:649/294  |  提交时间:2019/12/17
Kerosene  Supersonic combustion  Large eddy simulation  Skeletal mechanism  Scramjet  
Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
作者:  Fan WH(范文慧);  Zhong FQ(仲峰泉);  Ma SG(马素刚);  Zhang XY(张新宇)
浏览  |  Adobe PDF(4075Kb)  |  收藏  |  浏览/下载:297/86  |  提交时间:2020/03/11
Wall heat flux  Numerical simulation  Ethylene  Supersonic combustor