Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-10 of 20 Help

Filters            
Selected(0)Clear Items/Page:    Sort:
Local Piston Theory with Viscous Correction and Its Application 期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 3, 页码: 942-954
Authors:  Liu W(刘文);  Zhang CA(张陈安);  Han HQ;  Wang FM(王发民);  Zhang, CA (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1329Kb)  |  Favorite  |  View/Download：626/123  |  Submit date：2017/03/28
Hypersonic  Unsteady Aerodynamics  Piston Theory  Aeroelasticity  
Numerical study on initiation of oblique detonations in hydrogen-air mixtures with various equivalence ratios 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 卷号: 49, 页码: 130-134
Authors:  Zhang YN;  Gong JS;  Wang T(王涛);  Zhang, YN (reprint author), Beijing Power Machinery Res Inst, State Key Lab Laser Prop & Applicat, Beijing 100074, Peoples R China.
View  |  Adobe PDF(1388Kb)  |  Favorite  |  View/Download：519/133  |  Submit date：2016/03/21
Detonation  Hydrogen  Initiation  Hypersonic  
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：560/234  |  Submit date：2016/03/21
Aerodynamic Heating  Hypersonic  Shock Tunnel  Stanton Number  Sharp Cone  
Design of a pulse-type strain gauge balance for a long-test-duration hypersonic shock tunnel 期刊论文
SHOCK WAVES, 2016, 卷号: 26, 期号: 6, 页码: 835-844
Authors:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Wang, Y (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
Adobe PDF(2538Kb)  |  Favorite  |  View/Download：442/92  |  Submit date：2016/12/08
Hypersonic Shock Tunnel  Force Measurement  Strain Gauge Balance  
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：304/100  |  Submit date：2016/09/14
Hypersonic Flow  Aerodynamic Heating  Thermal Protection System  Forward-facing Cavity  
Design methodology for shape transition inlets based on constant contraction of discrete streamtubes 期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 卷号: 230, 期号: 8, 页码: 1496-1506
Authors:  Xiao YB(肖雅斌);  Yue LJ(岳连捷);  Ma SH;  Zhang XY(张新宇);  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100864, Peoples R China.
View  |  Adobe PDF(1353Kb)  |  Favorite  |  View/Download：442/105  |  Submit date：2016/09/14
Hypersonic Inlet  Shape Transition  Inward Turning  Scramjet  Design Method  
Theoretical calculation of mid-infrared spectra from hypersonic non-ablative sphere 会议论文
International Symposium on Infrared Technology and Application / International Symposium on Robot Sensing and Advanced Control, Beijing, PEOPLES R CHINA, MAY 09-11, 2016
Authors:  Wu J;  Yu XL(余西龙);  Zhu XJ;  Ma J;  Mao HX;  Wu, J (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Wu, J (reprint author), Sci & Technol Opt Radiat Lab, Beijing 100854, Peoples R China.
Adobe PDF(1160Kb)  |  Favorite  |  View/Download：297/89  |  Submit date：2017/05/12
Hypersonic  Mid-infrared  Atom  Diatomic Molecule  Partition-functions  Molecules  Air  
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.
Adobe PDF(860Kb)  |  Favorite  |  View/Download：459/200  |  Submit date：2015/04/28
Hypersonic Scramjet Test Tunnel  Nozzle  Aerodynamic Heating  Convective Heat Transfer  
Direct Numerical Simulation on Mach Number and Wall Temperature Effects in the Turbulent Flows of Flat-Plate Boundary Layer 期刊论文
COMMUNICATIONS IN COMPUTATIONAL PHYSICS, 2015, 卷号: 17, 期号: 1, 页码: 189-212
Authors:  Liang X;  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
Adobe PDF(860Kb)  |  Favorite  |  View/Download：795/251  |  Submit date：2015/06/12
Hypersonic  Directly Numerical Simulation  Compressibility Effects  Turbulent Boundary Layer  Strong Reynolds Analogy  
Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 8, 页码: 1980-1988
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Li GL(李广利);  Qu ZP(屈志朋);  Situ M;  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1426Kb)  |  Favorite  |  View/Download：899/296  |  Submit date：2013/09/27
Hypersonic  Flanking Air Inlet  Waverider  Computational Fluid Dynamics(Cfd)