Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-10 of 12 Help

Filters                                
Selected(0)Clear Items/Page:    Sort:
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.
Adobe PDF(1080Kb)  |  Favorite  |  View/Download：533/134  |  Submit date：2017/08/22
Aerodynamic Force And Moment Measurement  10° Half-angle Cone Model  Jf12  Real-gas Effects  Shock Tunnel  
Theories and technologies for duplicating hypersonic flight conditions for ground testing 期刊论文
NATIONAL SCIENCE REVIEW, 2017, 卷号: 4, 期号: 3, 页码: 290-U461
Authors:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing, Peoples R China.;  Jiang, ZL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing, Peoples R China.
Adobe PDF(1315Kb)  |  Favorite  |  View/Download：361/137  |  Submit date：2017/11/29
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.
Adobe PDF(514Kb)  |  Favorite  |  View/Download：485/99  |  Submit date：2016/12/08
Detonation Wave  Detonation Instability  Shock Wave  Chemical Reaction  
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.
Adobe PDF(1122Kb)  |  Favorite  |  View/Download：393/109  |  Submit date：2016/09/14
3d Shock/shock Interaction  Mach Interaction  Spatial Dimension Reduction  
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.
Adobe PDF(1162Kb)  |  Favorite  |  View/Download：371/96  |  Submit date：2016/09/14
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.
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  
Nonlinear saturation amplitude of cylindrical Rayleigh-Taylor instability 期刊论文
Chinese Physics B, 2014, 卷号: 23, 期号: 9, 页码: 94502
Authors:  Liu WH;  Yu CP(于长平);  Ye WH;  Wang LF;  Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
View  |  Adobe PDF(338Kb)  |  Favorite  |  View/Download：519/146  |  Submit date：2014/11/27
Nonlinear Saturation Amplitude  Rayleigh-taylor Instability  Cylindrical Interface  
Laser Diagnostics of Combustion Enhancement on a CH4/Air Bunsen Flame by Dielectric Barrier Discharge 期刊论文
CHINESE PHYSICS LETTERS, 2013, 卷号: 30, 期号: 8, 页码: 085203/1-085203/4
Authors:  Zhang SH(张少华);  Yu XL(余西龙);  Chen LH(陈立红);  Zhang XY(张新宇);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1970Kb)  |  Favorite  |  View/Download：867/276  |  Submit date：2013/09/27
Premixed Flames  Plasma  Methane  Mixtures  Planar Laser Induced Fluorescence  Laser Diagnostics  Flame Velocities  Emission Spectra  Dielectric Barrier Discharge  
Improvement of Baldwin-Lomax turbulence model for supersonic complex flows 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 3, 页码: 529–534
Authors:  Zhao R(赵瑞);  Yan C(阎超);  Yu J(于剑);  Li XL(李新亮);  Yan, C (reprint author), Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China.
Adobe PDF(1609Kb)  |  Favorite  |  View/Download：907/302  |  Submit date：2013/09/21
Baldwin-lomax Model  Boundary Layers  Computational Aerodynamics  Entropy  Supersonic Flows  Turbulence Models  
Application of the CE/SE Method to a Two-Phase Detonation Model in Porous Media 期刊论文
Chinese Physics Letters, 2011, 卷号: 28, 期号: 3, 页码: 30203
Authors:  Dong HF(董贺飞);  Hong T;  Zhang DL(张德良);  Hong, T (reprint author), Inst Appl Phys & Computat Math, Beijing 100094, Peoples R China
Adobe PDF(550Kb)  |  Favorite  |  View/Download：736/193  |  Submit date：2012/04/01
Transition