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Recent Progress of Microgravity Science Research in China 期刊论文
空间科学学报, 2022, 卷号: 42, 期号: 4, 页码: 772-785
作者:  Zhao JF(赵建福);  Du WF(杜王芳);  Kang Q(康琦);  Lan D(蓝鼎);  Li K(李凯);  Li WB(李伟斌);  Liu YC;  Luo XH;  Miao JY;  Wang QG;  Wang SF(王双峰);  Zhang T;  Zhang XW;  Zhang YH;  Zheng HQ
Adobe PDF(2911Kb)  |  收藏  |  浏览/下载:162/63  |  提交时间:2023/03/16
Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
作者:  Zhou, Lin;  Teng, Honghui;  Ng, Hoi Dick;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
Adobe PDF(6382Kb)  |  收藏  |  浏览/下载:219/32  |  提交时间:2021/11/01
Cellular detonation  Lead shock evolution  Multi-layer perceptron  Numerical simulations  
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:237/51  |  提交时间:2021/11/01
CO2-based mixture  flammability  laminar flame speed  flammable critical mixing ratio  transcritical power cycle  
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:280/55  |  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:383/57  |  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:322/169  |  提交时间:2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
作者:  Jiang ZL(姜宗林);  Li JP(李进平);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Yu HR(俞鸿儒)
Adobe PDF(1090Kb)  |  收藏  |  浏览/下载:252/101  |  提交时间:2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
作者:  Wang Q(汪球);  Luo K(罗凯);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟)
Adobe PDF(2057Kb)  |  收藏  |  浏览/下载:253/79  |  提交时间:2020/08/26
Shock tunnel  Detonation driver  Diaphragm  Dual ignition  High-enthalpy flow  
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)
Adobe PDF(9586Kb)  |  收藏  |  浏览/下载:645/293  |  提交时间:2019/12/17
Kerosene  Supersonic combustion  Large eddy simulation  Skeletal mechanism  Scramjet  
Non-premixed turbulent combustion modeling based on the filtered turbulent flamelet equation 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2019, 卷号: 63, 期号: 4, 页码: 6
作者:  Zhang J(张健);  Wang LP;  Guo YQ
Adobe PDF(1505Kb)  |  收藏  |  浏览/下载:170/52  |  提交时间:2020/05/18
turbulent combustion modeling  turbulent flamelet equation  large eddy simulation  non-premixed flame