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Experimental study of hysteresis and catastrophe in a cavity-based scramjet combustor 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 10, 页码: 118-133
Authors:  Zhang X(张旭);  Zhang QF(张启帆);  Wu ZJ(吴振杰);  Yue LJ(岳连捷);  Gao ZB(高占彪);  Luo WH(罗苇航);  Chen H(陈昊)
Adobe PDF(4834Kb)  |  Favorite  |  View/Download：33/3  |  Submit date：2023/07/17
Catastrophe  Cavity-based scramjet  Flame stabilization  Flame/shock interaction  Hysteresis  
Combustion Characteristic and Mechanism of a Mixture Working Fluid C3H8/CO2 期刊论文
JOURNAL OF THERMAL SCIENCE, 2021, 页码: 12
Authors:  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)  |  Favorite  |  View/Download：304/71  |  Submit date：2021/11/01
CO2-based mixture  flammability  laminar flame speed  flammable critical mixing ratio  transcritical power cycle  
Experimental Investigation on Flame Characterization and Temperature Profile of Single/Multiple Pool Fire in Cross Wind 期刊论文
JOURNAL OF THERMAL SCIENCE, 2020, 页码: 9
Authors:  Chen Z(陈阵);  Wei XL(魏小林);  Li T(李腾)
Adobe PDF(2122Kb)  |  Favorite  |  View/Download：300/108  |  Submit date：2020/09/07
pool fire  temperature profile  flame characteristic  kerosene  cross wind  
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
Authors:  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)  |  Favorite  |  View/Download：281/86  |  Submit date：2020/08/26
Shock tunnel  Detonation driver  Diaphragm  Dual ignition  High-enthalpy flow  
An efficient unstructured WENO method for supersonic reactive flows 期刊论文
ACTA MECHANICA SINICA, 2018, 卷号: 34, 期号: 4, 页码: 623-631
Authors:  Zhao WG;  Zheng HW(郑洪伟);  Liu FJ;  Shi XT;  Gao J;  Hu N;  Lv M;  Chen SC;  Zhao HD
View  |  Adobe PDF(3673Kb)  |  Favorite  |  View/Download：436/105  |  Submit date：2018/10/30
Supersonic reactive flows  Adaptive splitting scheme  Unstructured grids  WENO reconstruction  
Comparative study on aerodynamic heating under perfect and nonequilibrium hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 2, 页码: 624701
Authors:  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(763Kb)  |  Favorite  |  View/Download：584/239  |  Submit date：2016/03/21
Aerodynamic Heating  Hypersonic  Shock Tunnel  Stanton Number  Sharp Cone  
Development of the detonation-driven expansion tube for orbital speed experiments 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 4, 页码: 695-700
Authors:  Jiang ZL(姜宗林);  Wu B(吴波);  Gao YL;  Zhao W(赵伟);  Hu ZM(胡宗民);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(532Kb)  |  Favorite  |  View/Download：666/162  |  Submit date：2015/04/28
Detonation Driver  Shock-expansion Tube  High-enthalpy Flow  Test Flow