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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]
刘云峰 [6]
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Theoretical analysis for self-sharpening penetration of tungsten high-entropy alloy into steel target with elevated impact velocities
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 13
Authors:
Chen, Haihua
;
Zhang, Xianfeng
;
Liu, Chuang
;
Xiong, Wei
;
Tan, Mengting
;
Dai LH(戴兰宏)
Adobe PDF(2393Kb)
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Submit date:2021/08/03
Impact dynamics
Long-rod projectile
Tungsten high-entropy alloy (WHEA)
Self-sharpening penetration
Solid solution strengthening
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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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)
Adobe PDF(3477Kb)
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Submit date:2021/03/30
Temperature-sensitive paint
Time-resolved measurement
Hypersonic flow
Background radiation
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)
Adobe PDF(3790Kb)
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Submit date:2021/03/03
Hypersonics
Shock tunnels
Flow characteristics
Formation of stabilized oblique detonation waves in a combustor
期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
Authors:
Zhang ZJ(张子健)
;
Wen, Chihyung
;
Zhang WS(张文硕)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(3599Kb)
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Submit date:2021/03/03
Oblique detonation wave
Combustor
Oblique detonation engine
Normal detonation wave
Boundary layer separation
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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View/Download:355/177
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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 of a Mach 9 oblique detonation engine with fuel pre-injection
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
Authors:
Zhang ZJ(张子健)
;
Ma KF(马凯夫)
;
Zhang WS(张文硕)
;
Han X(韩鑫)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(2608Kb)
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Submit date:2020/11/30
Oblique detonation engine
Pre-injection
Detonative combustion
Mixing
Hydrogen
Coaxial Thermocouples for Heat Transfer Measurements in Long-Duration High Enthalpy Flows
期刊论文
SENSORS, 2020, 卷号: 20, 期号: 18, 页码: 18
Authors:
Zhang SZ(张仕忠)
;
Wang Q(汪球)
;
Li JP(李进平)
;
Zhang XY(张晓源)
;
Chen H(陈宏)
Adobe PDF(7131Kb)
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Submit date:2020/11/30
heat transfer measurement
coaxial thermocouple
long-duration
semi-infinite
high enthalpy
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)
Adobe PDF(1090Kb)
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Submit date:2020/11/30
hypervelocity
shock tunnel
detonation driver
flight condition
tailored condition
test facilities
Experimental Investigation of Hypervelocity Flow in an Expansion Tunnel
期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2776-2783
Authors:
Yuan CK(苑朝凯)
;
Zhou K(周凯)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(1471Kb)
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Submit date:2020/07/06