中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共12条，第1-10条 帮助

限定条件            
已选(0)清除 条数/页：   排序方式：
Numerical investigation of characteristic frequency excited highly underexpanded jets 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 63, 页码: 304-316
作者:  Li XP;  Fan E;  Yao W(姚卫);  Fan XJ(范学军);  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Fan, XJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
浏览  |  Adobe PDF(3588Kb)  |  收藏  |  浏览/下载：445/143  |  提交时间：2017/07/24
Fuel Jets  Underexpanded Jets  Jet Mixing Control  Excited Jets  Large Eddy Simulation  
Study on Flame Stabilization in a Dual-Mode Combustor Using Optical Measurements 期刊论文
JOURNAL OF PROPULSION AND POWER, 2015, 卷号: 31, 期号: 6, 页码: 1524-1531
作者:  Yuan YM(袁越明);  Zhang TC(张泰昌);  Yao W(姚卫);  Fan XJ(范学军);  Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(578Kb)  |  收藏  |  浏览/下载：480/133  |  提交时间：2016/03/21
A Slope Constrained 4th Order Multi-Moment Finite Volume Method with WENO Limiter 期刊论文
COMMUNICATIONS IN COMPUTATIONAL PHYSICS, 2015, 卷号: 18, 期号: 4, 页码: 901-930
作者:  Sun ZY;  Teng HH(滕宏辉);  Xiao F;  Xiao, F (reprint author), Tokyo Inst Technol, Dept Energy Sci, Midori Ku, 4259 Nagatsuta, Yokohama, Kanagawa 2268502, Japan.
浏览  |  Adobe PDF(1388Kb)  |  收藏  |  浏览/下载：339/129  |  提交时间：2016/01/08
Multi-moment Finite Volume Method  Weno  Flux Reconstruction  Compressible Flow  Conservative Method  Oscillation-suppressing  
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
作者:  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.
浏览  |  Adobe PDF(3301Kb)  |  收藏  |  浏览/下载：369/96  |  提交时间：2016/01/08
Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows  
Numerical study of oblique detonation wave initiation in a stoichiometric hydrogen-air mixture 期刊论文
PHYSICS OF FLUIDS, 2015, 卷号: 27, 期号: 9, 页码: 96101
作者:  Wang T;  Zhang YN;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Ng HD;  Wang, T (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1388Kb)  |  收藏  |  浏览/下载：403/129  |  提交时间：2016/01/08
Radical recombination in a hydrocarbon-fueled scramjet nozzle 期刊论文
Chinese Journal of Aeronautics, 2014, 卷号: 27, 期号: 6, 页码: 1413-1420
作者:  Zhang XY(张晓源);  Qin LZ;  Chen H(陈宏);  He XZ;  Liu Y;  Qin, LZ (reprint author), Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China.
浏览  |  Adobe PDF(1799Kb)  |  收藏  |  浏览/下载：424/93  |  提交时间：2015/03/11
Chemical Reactions  Nozzles  Performance Calculation  Radical  Recombination  
Quasi-One-Dimensional Multimodes Analysis for Dual-Mode Scramjet 期刊论文
JOURNAL OF PROPULSION AND POWER, 2014, 卷号: 30, 期号: 6, 页码: 1559-1567
作者:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Li F(李飞);  Zhang XY(张新宇);  Tian, L (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(7587Kb)  |  收藏  |  浏览/下载：589/136  |  提交时间：2014/12/18
Numerical investigation on the induction zone structure of the oblique detonation waves 期刊论文
Computers & Fluids, 2014, 卷号: 95, 页码: 127-131
作者:  Teng HH(滕宏辉);  Zhang YN;  Jiang ZL(姜宗林);  Teng, HH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1128Kb)  |  收藏  |  浏览/下载：1002/262  |  提交时间：2014/06/19
Detonation  Oblique Shock  Induction  Unstationary  
Theoretical analysis of effects of boundary layer bleed on scramjet thrust 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 10, 页码: 1952-1961
作者:  Yue LJ(岳连捷);  Xu XK(徐显坤);  Zhang XY(张新宇);  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(788Kb)  |  收藏  |  浏览/下载：879/258  |  提交时间：2013/10/23
Scramjet  Boundary Layer Bleed  Theoretical Analysis  Engine Thrust  
Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 卷号: 28, 期号: 1, 页码: 72-78
作者:  Li F(李飞);  Yu XL(余西龙);  Tong YG(仝颖刚);  Shen Y(沈岩);  Chen J(陈健);  Chen LH(陈立红);  Zhang XY(张新宇);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1235Kb)  |  收藏  |  浏览/下载：1290/414  |  提交时间：2013/07/30
Scramjet  Kerosene Fuel  Plasma Torch  Ignition