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Initiation structure of oblique detonation waves behind conical shocks 期刊论文
PHYSICS OF FLUIDS, 2017, 卷号: 29, 期号: 8
Authors:  Yang PF(杨鹏飞);  Ng, Hoi Dick;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Teng, HH (reprint author), Beijing Inst Technol, Sch Aerosp Engn, Dept Mech, Beijing 100081, Peoples R China.
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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
Authors:  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.
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Fuel Jets  Underexpanded Jets  Jet Mixing Control  Excited Jets  Large Eddy Simulation  
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.
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Detonation Wave  Detonation Instability  Shock Wave  Chemical Reaction  
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
Authors:  Wang ZP(王知溥);  Li F(李飞);  Gu HS;  Yu XL(余西龙);  Zhang XY(张新宇);  Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas  
Evolution of cellular structures on oblique detonation surfaces 期刊论文
COMBUSTION AND FLAME, 2015, 卷号: 162, 期号: 2, 页码: 470-477
Authors:  Teng HH(滕宏辉);  Ng HD;  Li K(李康);  Luo CT(罗长童);  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.
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Detonation  Instability  Cellular Structure  Transverse Wave  Numerical Simulations  
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
Authors:  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.
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Chemical Reactions  Nozzles  Performance Calculation  Radical  Recombination  
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
Authors:  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.
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Detonation  Oblique Shock  Induction  Unstationary  
Numerical study on unstable surfaces of oblique detonations 期刊论文
JOURNAL OF FLUID MECHANICS, 2014, 卷号: 744, 页码: 111-128
Authors:  Teng, Hong Hui;  Jiang, Zong Lin;  Ng, Hoi Dick;  Teng, HH (reprint author),Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
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Compressible Flows  Detonation Waves  
Effects of different product phases in aluminum dust detonation modeling 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 11, 页码: 2178-2185
Authors:  Teng HongHui;  Jiang ZongLin;  Teng, HH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Detonation  Aluminum  Multiphase  
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
Authors:  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)  |  Favorite  |  View/Download：887/262  |  Submit date：2013/10/23
Scramjet  Boundary Layer Bleed  Theoretical Analysis  Engine Thrust