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Knowledge Management System of Institue of Mechanics, CAS
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刘云峰 [10]
姜宗林 [10]
罗长童 [4]
胡宗民 [4]
苑朝凯 [4]
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Indexed By:CSCD
Creator:刘云峰
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Creator:姜宗林
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一维与二维爆轰传播的时空关联特性数值研究
期刊论文
力学学报, 2021, 卷号: 53, 期号: 07, 页码: 2069-2078
Authors:
张文硕
;
杨鹏飞
;
姜宗林
;
刘云峰
Adobe PDF(1701Kb)
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Submit date:2021/08/25
斜爆轰
活塞
时空关联
基元反应模型
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)
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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)
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Submit date:2021/03/30
Temperature-sensitive paint
Time-resolved measurement
Hypersonic flow
Background radiation
On theory and methods for advanced detonation-driven hypervelocity shock tunnels
期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors:
Jiang ZL(姜宗林)
;
Li JP(李进平)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Yu HR(俞鸿儒)
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Submit date:2020/11/30
hypervelocity
shock tunnel
detonation driver
flight condition
tailored condition
test facilities
Spectral measurements of hypervelocity flow in an expansion tunnel
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
Authors:
Yuan CK(苑朝凯)
;
Zhou K(周凯)
;
Liu YF(刘云峰)
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
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Submit date:2019/04/11
Spectral measurement
Hypervelocity flow
Radiation
Expansion tunnel
Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel
期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
Authors:
Liu YF(刘云峰)
;
Wang YP(汪运鹏)
;
Yuan CK(苑朝凯)
;
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
;
Liu, YF (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:2017/08/22
Aerodynamic Force And Moment Measurement
10° Half-angle Cone Model
Jf12
Real-gas Effects
Shock Tunnel
振动激发对高超声速气动力/热影响
期刊论文
力学学报, 2017, 卷号: 49, 期号: 03, 页码: 616-626
Authors:
张子健
;
刘云峰
;
姜宗林
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Submit date:2017/12/22
振动激发
气动力/热
边界层
高温气体效应
长试验时间激波风洞测力技术研究
期刊论文
力学学报, 2016, 卷号: 48, 期号: 3, 页码: 545-556
Authors:
汪运鹏
;
刘云峰
;
苑朝凯
;
罗长童
;
王春
;
胡宗民
;
韩桂来
;
赵伟
;
姜宗林
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Adobe PDF(8800Kb)
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Submit date:2016/12/16
Shock Tunnel
Long-test Duration
Force Measurement
Strain-gaged Balance
高超声速风洞实验数据的多维空间相关理论与关联方法
期刊论文
中国科学: 物理学 力学 天文学, 2015, 卷号: 45, 期号: 12, 页码: 124705
Authors:
姜宗林
;
罗长童
;
胡宗民
;
刘云峰
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Adobe PDF(3524Kb)
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Submit date:2016/01/07
长试验时间爆轰驱动激波风洞技术研究
期刊论文
力学学报, 2012, 卷号: 44, 期号: 5, 页码: 824-831
Authors:
姜宗林
;
李进平
;
赵伟
;
刘云峰
;
俞鸿儒
Adobe PDF(2350Kb)
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Submit date:2013/01/16
高超声速飞行
反向爆轰驱动激波风洞
长试验时间
高温气体流动