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汪球 [5]
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Indexed By:EI
Creator:汪球
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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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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:305/111
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Submit date:2021/11/01
Non-equilibrium plasma
Plasma-assisted ignition
Plasma-assisted combustion
Aerospace engine
Combustor
Extreme condition
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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View/Download:273/52
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Submit date:2021/11/01
Potential Agricultural and Biomedical Applications of Cold Atmospheric Plasma-Activated Liquids With Self-Organized Patterns Formed at the Interface
期刊论文
IEEE TRANSACTIONS ON PLASMA SCIENCE, 2020, 卷号: 48, 期号: 10, 页码: 3455-3471
Authors:
Chen ZT
;
Xu RG
;
Chen PJ
;
Wang Q(汪球)
Adobe PDF(5426Kb)
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View/Download:472/297
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Submit date:2020/11/30
Plasmas
Liquids
Discharges (electric)
Anodes
Surface discharges
Conductivity
Cold atmospheric plasma (CAP)
food safety
plasma agriculture
plasma medicine
plasma-treated liquids
self-organized pattern (SOP)
Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
Authors:
Wang Q(汪球)
;
Luo K(罗凯)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
Adobe PDF(2057Kb)
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Submit date:2020/08/26
Shock tunnel
Detonation driver
Diaphragm
Dual ignition
High-enthalpy flow
Performance of Copper Calorimeter for Heat Transfer Measurement in High Enthalpy Shock Tunnel
期刊论文
JOURNAL OF THERMAL SCIENCE, 2018, 卷号: 27, 期号: 4, 页码: 373-381
Authors:
Wang Q(汪球)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Jiang ZL(姜宗林)
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View/Download:722/144
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Submit date:2018/10/30
copper calorimeter
high enthalpy shock tunnel
heat transfer
hypersonic