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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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姜宗林 [8]
俞鸿儒 [2]
刘云峰 [2]
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高超声速高焓条件下的内嵌式温敏漆测量方法
期刊论文
力学学报, 2022, 卷号: 54, 期号: 01, 页码: 48-58
Authors:
苑朝凯
;
姜宗林
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Submit date:2022/03/16
温敏漆
热流密度场
辐射效应
高超声速流动
辨识方法
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
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)
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Submit date:2021/03/03
Hypersonics
Shock tunnels
Flow characteristics
高超声速喷管设计理论与方法
期刊论文
力学进展, 2020, 卷号: 51, 期号: 02, 页码: 257-294
Authors:
汪运鹏
;
姜宗林
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Submit date:2021/01/29
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)
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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
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
Theories and technologies for duplicating hypersonic flight conditions for ground testing
期刊论文
NATIONAL SCIENCE REVIEW, 2017, 卷号: 4, 期号: 3, 页码: 290-U461
Authors:
Jiang ZL(姜宗林)
;
Yu HR(俞鸿儒)
;
Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing, Peoples R China.
;
Jiang, ZL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing, Peoples R China.
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Submit date:2017/11/29
高焓激波风洞喷管流场非平衡特性研究
期刊论文
空气动力学学报, 2015, 卷号: 33, 期号: 1, 页码: 66-71
Authors:
汪球
;
赵伟
;
滕宏辉
;
姜宗林
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Submit date:2015/11/02
爆轰驱动
非平衡
焓值
激波风洞