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姜宗林 [11]
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Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition
期刊论文
AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17
Authors:
Zhang WS(张文硕)
;
Zhang, Zijian
;
Jiang ZL(姜宗林)
;
Han X(韩信)
;
Liu YF(刘云峰)
;
Wang C(王春)
Adobe PDF(15045Kb)
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Submit date:2022/01/24
Experimental study on shock wave control in high-enthalpy hypersonic flow by using SparkJet actuator
期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 416-425
Authors:
Xie, Wei
;
Luo, Zhenbing
;
Zhou, Yan
;
Gao, Tianxiang
;
Wu, Yun
;
Wang Q(汪球)
Adobe PDF(8485Kb)
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View/Download:144/75
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Submit date:2022/10/25
SparkJet
High-enthalpy hypersonic flow
Shock control
Shock-on-shock interaction
Air supply
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors:
Li, Mengzhe
;
Wang, Zhikai
;
Xu, Rongguang
;
Zhang, Xiaoliang
;
Chen, Zhitong
;
Wang Q(汪球)
Adobe PDF(8841Kb)
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View/Download:293/110
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Submit date:2021/11/01
Non-equilibrium plasma
Plasma-assisted ignition
Plasma-assisted combustion
Aerospace engine
Combustor
Extreme condition
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors:
Zhou GX(周功喜)
;
Zhang X(张旭)
;
Li JP(李进平)
;
Zhang XY(张晓源)
;
Zhang SZ(张仕忠)
;
Lin X(林鑫)
;
Li F(李飞)
;
Chen H(陈宏)
;
Yue LJ(岳连捷)
;
Yu XL(余西龙)
Adobe PDF(4108Kb)
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Submit date:2021/09/07
High mach number scramjet
Circular cross-section
TDLAS
Multi-view simultaneous imaging
POD
Numerical and experimental study on high-speed hydrogen-oxygen combustion gas flow and aerodynamic heating characteristics
期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 7, 页码: 11
Authors:
Yu JP(于江鹏)
;
Li JP(李进平)
;
Wang Q(汪球)
;
Zhang SZ(张仕忠)
;
Zhang XY(张晓源)
Adobe PDF(3271Kb)
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Submit date:2021/11/01
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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View/Download:296/65
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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:
Jiang ZL(姜宗林)
;
Hu ZM(胡宗民)
;
Wang YP(汪运鹏)
;
Han GL(韩桂来)
Adobe PDF(1129Kb)
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Submit date:2021/03/30
High-enthalpy flow
Hypersonic wind tunnel
Aerospace vehicle
Aerodynamic balance
Heat flux sensor
Optical measurement technique
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Ma SH(马生虎)
;
Zhang QF(张启帆)
;
Zhang, Peng
;
Zhang XY(张新宇)
Adobe PDF(3937Kb)
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Submit date:2021/03/30
Adverse pressure gradient
Back pressure
Hysteresis effects
Non-uniform flow
Shock train
Space-Time Conservation Element and Solution Element Method and Its Applications
期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 12, 页码: 5408-5430
Authors:
Jiang YZ
;
Wen CY
;
Zhang DL(张德良)
Adobe PDF(6207Kb)
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Submit date:2021/02/09
Synthesis and characterization of light-weight porous ceramics used in the transpiration cooling
期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 177, 页码: 438-445
Authors:
Zhang, Bo
;
Huang, Jie
;
Li, Weijie
;
Huang, Haiming
;
Zhao, Huanyu
;
Peng JL(彭锦龙)
Adobe PDF(8097Kb)
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Submit date:2021/03/30
Carbon fiber-reinforced silicon carbide porous ceramics
Permeability
Oxyacetylene flame test
Transpiration cooling