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Knowledge Management System of Institue of Mechanics, CAS
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Date Issued:2015
Community:高温气体动力学国家重点实验室
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Numerical study of combustion and convective heat transfer of a Mach 2.5 supersonic combustor
期刊论文
APPLIED THERMAL ENGINEERING, 2015, 卷号: 89, 页码: 883-896
Authors:
Wang X
;
Zhong FQ(仲峰泉)
;
Gu HB(顾宏斌)
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2016/01/08
Supersonic Combustor
Convective Heat Transfer
Numerical Study
Wall Heat Flux
Wave system fitting: A new method for force measurements in shock tunnels with long test duration
期刊论文
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2015, 卷号: 62-63, 页码: 2841-2848
Authors:
Luo CT(罗长童)
;
Wang YP(汪云鹏)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
;
Luo, CT (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:2016/01/07
Aerodynamic Force Measurements
Strain Gauge Balance
Inertia Compensation
Signal Decomposition
Accelerometer-free
Shock Tunnels
Tunable diode laser absorption spectroscopy measurements of high-pressure ammonium dinitramide combustion
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 45, 页码: 140-149
Authors:
Yao, Zhaopu
;
Zhang, Wei
;
Wang, Meng
;
Chen, Jun
;
Shen, Yan
;
Wei, Yanming
;
Yu XL(余西龙)
;
Li F(李飞)
;
Ceng H(曾徽)
;
Yu, XL (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:2015/10/21
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
Authors:
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.
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Submit date:2016/01/08
Mechanisms for non-ideal flow in low-power arc-heated supersonic nozzles
期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 4, 页码: 500-511
Authors:
Wu CK(吴承康)
;
Pan WX(潘文霞)
;
Meng X(孟显)
;
Wang, Hai-Xing
;
Wu, CK (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:2015/10/21
Arc-heated Supersonic Jet
Low-power
Real Flow
Viscosity Effect
Low Reynolds Number
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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Submit date:2015/06/12
Scramjet
Dual-mode Combustor
Divergent Angle
Cavity Location
Combustion Efficiency
Tdlas
Study and prediction for the fire resistance of acid corroded intumescent coating
会议论文
9th International Symposium on Safety Science and Technology (ISSST), Beijing, PEOPLES R CHINA, NOV 04-06, 2014
Authors:
Wang J
;
Song WH
;
Zhang M
;
Chen Z(陈阵)
;
Song, WH (reprint author), Tianjin Polytech Univ, Environm & Chem Coll, Tianjin 300387, Peoples R China.
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Submit date:2016/06/28