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基于主动射流控制的高超声速进气道再起动性能研究(英文) 期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:  靳一超;  姚卫
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高超声速进气道  不起动  再起动  主动射流  流动控制  
Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
Adobe PDF(1806Kb)  |  Favorite  |  View/Download:289/60  |  Submit date:2021/05/17
Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
Modeling De-NOx by Injection Ammonia in High Temperature Zone of Cement Precalciner 期刊论文
JOURNAL OF THERMAL SCIENCE, 2020
Authors:  Zhang LY(张乐宇);  Wei XL(魏小林);  Zhang ZX;  Li S(李森)
Adobe PDF(1220Kb)  |  Favorite  |  View/Download:280/145  |  Submit date:2020/12/28
cement precalciner  SELECTIVE NONCATALYTIC REDUCTION  coal combustion  NUMERICAL-SIMULATION  CaCO3 decomposition  SNCR  high temperature zone  COMBUSTION  SNCR  OPTIMIZATION  
Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177
Authors:  Yao W(姚卫)
View  |  Adobe PDF(9586Kb)  |  Favorite  |  View/Download:658/296  |  Submit date:2019/12/17
Kerosene  Supersonic combustion  Large eddy simulation  Skeletal mechanism  Scramjet  
Hypersonic I-shaped aerodynamic configurations 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2018, 卷号: 61, 期号: 2, 页码: 24722
Authors:  Cui K(崔凯);  Xiao Y(肖尧);  Xu YZ;  Li GL
View  |  Adobe PDF(665Kb)  |  Favorite  |  View/Download:437/132  |  Submit date:2018/10/30
Effect of uniform blowing or suction on hypersonic spatially developing turbulent boundary layers 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 6, 页码: 664702
Authors:  Chen Z(陈哲);  Yu ZP(于长平);  Li L(李理);  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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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.
View  |  Adobe PDF(1162Kb)  |  Favorite  |  View/Download:343/87  |  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.
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Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows