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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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High-Pressure Capturing Wing Configurations
期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 6, 页码: 1909-1919
Authors:
Cui K(崔凯)
;
Li GL
;
Xiao Y(肖尧)
;
Xu YZ
;
Cui,K(reprint author), Chinese Acad Sci, Inst Mech
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Submit date:2017/07/24
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.
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Submit date:2017/03/28
Hypersonic
Unsteady Aerodynamics
Piston Theory
Aeroelasticity
Characterization of flame stabilization modes in an ethylene-fueled supersonic combustor using time-resolved CH* chemiluminescence
期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2017, 卷号: 36, 期号: 2, 页码: 2919-2925
Authors:
Yuan YM(袁越明)
;
Zhang TC(张泰昌)
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Zhang P(张鹏)
;
Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Beijing 100190, PR, Peoples R China.
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Submit date:2017/12/27
Supersonic Combustion
Flame Stabilization
Stagtnation Temperature
Gloabal Equivalence Ratio
Ch** Ch*emiluminesenCh*e
Starting Process in a Large-Scale Shock Tunnel
会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
Authors:
Wang YP
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Wang, YP (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2016/06/28
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.
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View/Download:365/93
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Submit date:2016/09/14
Dual-mode Scramjet
Engine Performance
Thrust
Optimization
Heat Release Distribution
Simulated Annealing Algorithm
Heat Transfer and Mode Transition for Laser Ablation Subjected to Supersonic Airflow
期刊论文
CHINESE PHYSICS LETTERS, 2016, 卷号: 33, 期号: 1, 页码: 14201
Authors:
Huang YH
;
Song HW(宋宏伟)
;
Huang CG(黄晨光)
;
Song, HW (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China.
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Submit date:2016/03/21
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
Authors:
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.
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Submit date:2016/03/21
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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View/Download:398/105
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Submit date:2016/01/08
Boundary Layer Control
Boundary Layer Heat Flow
Shock Wave Interactions
Separated Flows
Combustion of Vaporized Kerosene in Supersonic Model Combustors with Dislocated Dual Cavities
期刊论文
Journal of Propulsion and Power, 2014, 卷号: 30, 期号: 5, 页码: 1152-1160
Authors:
Zhang TC(张泰昌)
;
Wang J(王晶)
;
Fan XJ(范学军)
;
Zhang P
;
Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2014/11/27
Blowout Limits of Cavity-Stabilized Flame of Supercritical Kerosene in Supersonic Combustors
期刊论文
Journal of Propulsion and Power, 2014, 卷号: 30, 期号: 5, 页码: 1161-1166
Authors:
Zhang TC(张泰昌)
;
Wang J(王晶)
;
Qi L
;
Fan XJ(范学军)
;
Zhang P
;
Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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View/Download:788/257
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Submit date:2014/11/27