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State Key ... [9]
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汪球 [9]
李进平 [4]
罗凯 [3]
赵伟 [3]
李逸翔 [2]
栗继伟 [2]
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Creator:汪球
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Date Issued:2021
Community:高温气体动力学国家重点实验室
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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:147/76
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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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Submit date:2021/11/01
Non-equilibrium plasma
Plasma-assisted ignition
Plasma-assisted combustion
Aerospace engine
Combustor
Extreme condition
高超声速MHD球头激波脱体距离理论求解
期刊论文
力学学报, 2021, 卷号: 53, 期号: 09, 页码: 2493-2500
Authors:
李逸翔
;
汪球
;
罗凯
;
李进平
;
赵伟
Adobe PDF(1290Kb)
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Submit date:2021/11/12
高超声速
磁流体动力学
激波脱体距离
流动控制
Effects of Cowl-Induced Expansion on the Wave Complex Induced by Oblique Detonation Wave Reflection
期刊论文
PROCESSES, 2021, 卷号: 9, 期号: 7, 页码: 10
Authors:
Wang, Aifeng
;
Shang JH(尚佳豪)
;
Wang Q(汪球)
;
Wang KL(王宽亮)
Adobe PDF(3951Kb)
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Submit date:2021/08/16
oblique detonation
asymmetric
nozzle
reflection
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
基于高温气体效应的磁流体流动控制研究进展
期刊论文
力学学报, 2021, 卷号: 53, 期号: 06, 页码: 1515-1531
Authors:
罗凯
;
汪球
;
李逸翔
;
李进平
;
赵伟
Adobe PDF(12949Kb)
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Submit date:2021/11/12
高超声速
高温真实气体效应
磁流体动力学
流动控制
气动力/热
Evolution of heat transfer at the stagnation point during the detached bow shock establishment
期刊论文
SHOCK WAVES, 2021, 页码: 8
Authors:
Wang Q(汪球)
;
Li JP(李进平)
;
Luo K(罗凯)
;
Li JW(栗继伟)
;
Zhao W(赵伟)
Adobe PDF(1158Kb)
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Submit date:2021/05/17
Hypersonic
Aerodynamic heating
Detached bow shock
Shock tube
expansion tube
Fast-response oxygen sensitive transparent coating for inner pressure ratiometric optical mapping
期刊论文
JOURNAL OF MATERIALS CHEMISTRY C, 2021, 卷号: 9, 期号: 11, 页码: 3919-3927
Authors:
Yang Di
;
Li JW(栗继伟)
;
Ren Junkai
;
Wang Qinglin
;
Zhou Shuyun
;
Wang Q(汪球)
;
Xie Zheng
;
Qu Xiaozhong
Adobe PDF(4555Kb)
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Submit date:2021/05/06
一种基于激波管的TDLAS测温的高温标定设备及方法
专利
发明专利. 一种基于激波管的TDLAS测温的高温标定设备及方法, 专利号: ZL202010070139.9, 申请日期: 2020-01-21, 授权日期: 2021-03-02
Inventors:
李飞
;
林鑫
;
汪球
;
余西龙
Adobe PDF(667Kb)
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Submit date:2021/11/23