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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  
Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel 期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
Authors:  Liu YF(刘云峰);  Wang YP(汪运鹏);  Yuan CK(苑朝凯);  Luo ZT(罗长童);  Jiang ZL(姜宗林);  Liu, YF (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Aerodynamic Force And Moment Measurement  10° Half-angle Cone Model  Jf12  Real-gas Effects  Shock Tunnel  
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.
Adobe PDF(763Kb)  |  Favorite  |  View/Download：551/232  |  Submit date：2016/03/21
Aerodynamic Heating  Hypersonic  Shock Tunnel  Stanton Number  Sharp Cone  
Theoretical solutions to three-dimensional asymmetrical shock/shock interaction 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 8, 页码: 1208-1216
Authors:  Xiang GX(项高翔);  Wang C(王春);  Hu ZM(胡宗民);  Li XD;  Jiang ZL(姜宗林);  Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
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3d Asymmetrical Shock/shock Interaction  Spatial-dimension Reduction  Mach Reflection  Flow Field  Theoretical Analysis  
Study on Mach stems induced by interaction of planar shock waves on two intersecting wedges 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 3, 页码: 362-368
Authors:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(滕宏辉);  Yang Y;  Jiang ZL(姜宗林);  Wang, C (reprint author), Chinese Acad Sci, Inst Mech, 15 Beisihuan Xi Rd, Beijing 100190, Peoples R China.
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3d Shock/shock Interaction  Mach Interaction  Spatial Dimension Reduction  
Effect of uniform blowing or suction on hypersonic spatially developing turbulent boundary layers 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 6, 页码: 664702
Authors:  Chen Z(陈哲);  Yu ZP(于长平);  Li L(李理);  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Numerical investigation on the thermal protection mechanism for blunt body with forward-facing cavity 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 7, 页码: 1120-1129
Authors:  Li, XD;  Hu ZM(胡宗民);  Jiang ZL(姜宗林);  Hu, ZM (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(2496Kb)  |  Favorite  |  View/Download：298/98  |  Submit date：2016/09/14
Hypersonic Flow  Aerodynamic Heating  Thermal Protection System  Forward-facing Cavity  
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  
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.
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Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows  
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.
Adobe PDF(532Kb)  |  Favorite  |  View/Download：649/157  |  Submit date：2015/04/28
Detonation Driver  Shock-expansion Tube  High-enthalpy Flow  Test Flow