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Language:英语
Document Type:期刊论文
Community:高温气体动力学国家重点实验室
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Combustion dynamics of high Mach number scramjet under different inflow thermal nonequilibrium conditions
期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 208, 页码: 281-295
Authors:
Ao Y(敖彧)
;
Wu K(吴坤)
;
Lu, Hongbo
;
Ji, Feng
;
Fan XJ(范学军)
Adobe PDF(11339Kb)
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Submit date:2023/06/15
Hypervelocity combustion
Thermal nonequilibrium
Two-temperature model
Numerical simulation
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel
期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(2434Kb)
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View/Download:329/88
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Submit date:2022/08/23
Aerodynamic Coefficients
Two Stage to Orbit
Aerodynamic Performance
Hypersonic Flight
Hypersonic Wind Tunnels
Solenoid Valves
Oblique Shock
Pneumatic Actuator
Hypersonic Flows
Computer Aided Engineering
Numerical study of high temperature non-equilibrium effects of double-wedge in hypervelocity flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 124, 页码: 17
Authors:
Dai, Chunliang
;
Sun, Bo
;
Zhuo, Changfei
;
Zhou, Shengbing
;
Zhou, Changsheng
;
Yue LJ(岳连捷)
Adobe PDF(6822Kb)
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Submit date:2022/07/18
Hypervelocity double-wedge flow
High temperature non-equilibrium effects
Laminar and turbulence flow
Shock wave interaction
Shock wave
boundary layer interaction
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:
Yao W(姚卫)
;
Liu H(刘杭)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
Adobe PDF(2954Kb)
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Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
Reduction of surface friction drag in scramjet engine by boundary layer combustion
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
Authors:
Xue, Rui
;
Zheng, Xing
;
Yue LJ(岳连捷)
;
Zhang, Qian
;
He, Xin
;
Yang, Jing
;
Weng, Chao
;
Li, Zhihao
Adobe PDF(5483Kb)
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Submit date:2022/10/25
Boundary layer combustion
Skin-friction reduction
Supersonic combustion
Scramjet engine
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)
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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
Noise reduction for temperature-sensitive paint measurement contaminated by strong background radiation in a high enthalpy hypersonic tunnel
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 7
Authors:
Peng, Di
;
Liu, Xu
;
Jiao, Lingrui
;
Li, Ziyan
;
Wen, Xin
;
Yuan CK(苑朝凯)
;
Han GL(韩桂来)
;
Liu YF(刘云峰)
;
Liu, Yingzheng
;
Jiang ZL(姜宗林)
Adobe PDF(3477Kb)
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Submit date:2021/03/30
Temperature-sensitive paint
Time-resolved measurement
Hypersonic flow
Background radiation
Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
Authors:
Yuan CK(苑朝凯)
;
Jiang ZL(姜宗林)
Adobe PDF(3790Kb)
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Submit date:2021/03/03
Hypersonics
Shock tunnels
Flow characteristics
Formation of stabilized oblique detonation waves in a combustor
期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
Authors:
Zhang ZJ(张子健)
;
Wen, Chihyung
;
Zhang WS(张文硕)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(3599Kb)
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Submit date:2021/03/03
Oblique detonation wave
Combustor
Oblique detonation engine
Normal detonation wave
Boundary layer separation
Direct numerical simulation of supersonic turbulent expansion corner with shock impingement
期刊论文
Physics of Fluids, 2021, 卷号: 33, 页码: 105104
Authors:
Zhang ZG(张志刚)
;
Tong FL(童福林)
;
Duan JY(段俊亦)
;
Li XL(李新亮)
Adobe PDF(8048Kb)
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Submit date:2021/11/23