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Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
Authors:  Tong FL(童福林);  Sun D(孙栋);  Li XL(李新亮)
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Direct numerical simulation  Low-frequency unsteadiness  Shock waves  Turbulent boundary layer  Wavy-wall  
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)
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pool fire  temperature profile  flame characteristic  kerosene  cross wind  
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
Authors:  Yao W(姚卫)
Adobe PDF(9586Kb)  |  Favorite  |  View/Download:673/301  |  Submit date:2019/12/17
Kerosene  Supersonic combustion  Large eddy simulation  Skeletal mechanism  Scramjet  
Effects of dimensional wall temperature on velocity-temperature correlations in supersonic turbulent channel flow of thermally perfect gas 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2019, 卷号: 62, 期号: 6, 页码: AR64711
Authors:  Chen XP;  Li XL(李新亮);  Zhu ZC
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direct numerical simulation  velocity-temperature correlation  supersonic flow  channel flow  thermally perfect gas  strong Reynolds analogy  
Shock relations in gases of heterogeneous thermodynamic properties 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
Authors:  Hu ZM(胡宗民);  Zhou K(周凯);  Peng J(彭俊);  Li JP(李进平);  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.
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Shock Wave  Imperfect Gas  Heterogeneous  Theoretical Solution  
Sufficiently diffused attachment of nitrogen arc by gasdynamic action 期刊论文
Theoretical and Applied Mechanics Letters, 2016, 卷号: 6, 期号: 6, 页码: 293-296
Authors:  Pan WX(潘文霞);  Chen LW(陈乐文);  Meng X(孟显);  Zhang Y(张勇);  Wu CK(吴承康);  Pan WX(潘文霞)
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Pure Nitrogen Arcdiffused Arc Root Attachmentgas Dynamic Expanding actionArc Channel Structureworking Paramete  
Theoretical approach to one-dimensional detonation instability 期刊论文
APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2016, 卷号: 37, 期号: 9, 页码: 1231-1238
Authors:  Wang C(王春);  Xiang GX(项高翔);  Jiang ZL(姜宗林);  Wang, C (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Detonation Wave  Detonation Instability  Shock Wave  Chemical Reaction  
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
A quasi-one-dimensional model for hypersonic reactive flow along the stagnation streamline 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2016, 卷号: 29, 期号: 6, 页码: 1517-1526
Authors:  Chen S;  Sun QH(孙泉华)
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Aerothermal characteristics of bleed slot in hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 卷号: 58, 期号: 10, 页码: 104703
Authors:  Yue LJ(岳连捷);  Lu HB;  Xu X;  Chang XY;  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(3301Kb)  |  Favorite  |  View/Download:400/105  |  Submit date:2016/01/08
Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows