Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-6 of 6 Help

Filters                        
Selected(0)Clear Items/Page:    Sort:
Study of coupled effect of impingement jet cooling of kerosene with solid structure 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2019, 卷号: 62, 期号: 11, 页码: 2021-2028
Authors:  Du MM(杜蒙蒙);  Zhong FQ(仲峰泉);  Xing YF(邢云绯);  Zhang XY(张新宇)
View  |  Adobe PDF(2806Kb)  |  Favorite  |  View/Download：388/99  |  Submit date：2020/03/21
impingement jet cooling  hydrocarbon fuel  heat transfer enhancement  fluid-solid coupling  
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.
View  |  Adobe PDF(1654Kb)  |  Favorite  |  View/Download：376/94  |  Submit date：2017/10/25
Shock Wave  Imperfect Gas  Heterogeneous  Theoretical Solution  
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.
View  |  Adobe PDF(995Kb)  |  Favorite  |  View/Download：509/124  |  Submit date：2016/12/08
3d Asymmetrical Shock/shock Interaction  Spatial-dimension Reduction  Mach Reflection  Flow Field  Theoretical Analysis  
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.
View  |  Adobe PDF(2496Kb)  |  Favorite  |  View/Download：306/101  |  Submit date：2016/09/14
Hypersonic Flow  Aerodynamic Heating  Thermal Protection System  Forward-facing Cavity  
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：653/158  |  Submit date：2015/04/28
Detonation Driver  Shock-expansion Tube  High-enthalpy Flow  Test Flow  
Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 3, 页码: 470-475
Authors:  Xing YF(邢云绯);  Zhong FQ(仲峰泉);  Li DX(李东霞);  Zhang XY(张新宇);  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(860Kb)  |  Favorite  |  View/Download：462/202  |  Submit date：2015/04/28
Hypersonic Scramjet Test Tunnel  Nozzle  Aerodynamic Heating  Convective Heat Transfer