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Knowledge Management System of Institue of Mechanics, CAS
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姜宗林 [2]
张启帆 [2]
栗继伟 [2]
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Funding Organization:National Natural Science Foundation of China
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Near-field relaxation subsequent to the onset of oblique detonations with a two-step kinetic model
期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 9, 页码: 11
Authors:
Teng, Honghui
;
Ng, Hoi Dick
;
Yang PF(杨鹏飞)
;
Wang, Kuanliang
Adobe PDF(5463Kb)
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View/Download:185/36
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Submit date:2022/01/13
The effects of particle size on flameless combustion characteristics and NOx emissions of semi-coke with coal
期刊论文
FUEL, 2021, 卷号: 297, 页码: 13
Authors:
Ding, Hongliang
;
Ouyang, Ziqu
;
Zhang, Xiaoyu
;
Zhu SJ(朱书骏)
Adobe PDF(5100Kb)
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View/Download:337/95
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Submit date:2021/06/15
Particle size
Self-preheating
Flameless combustion
NOx emissions
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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View/Download:299/105
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Submit date:2021/05/06
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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View/Download:278/57
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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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View/Download:418/72
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Submit date:2021/03/03
Hypersonics
Shock tunnels
Flow characteristics
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors:
Tong XT(仝晓通)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(8067Kb)
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View/Download:413/75
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Submit date:2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow
Construction of bi-layer biluminophore fast-responding pressure sensitive coating for non-contact unsteady aerodynamic testing
期刊论文
POLYMER TESTING, 2019, 卷号: 77, 页码: 8
Authors:
Yang D
;
Ren JK
;
Li JW(栗继伟)
;
Wang QL
;
Wang Q(汪球)
;
Xie Z
;
Qu XZ
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  |  
Adobe PDF(2608Kb)
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View/Download:1045/799
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Submit date:2019/11/25
Pressure sensitive paint (PSP)
Bi-layer structured coating
Fast-response
Self-referenced measurement
External-Compression Supersonic Inlet Free from Violent Buzz
期刊论文
AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523
Authors:
Chen H
;
Tan H
;
Liu YZ
;
Zhang QF(张启帆)
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View/Download:288/99
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Submit date:2019/09/09
Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules
期刊论文
ACTA ASTRONAUTICA, 2019, 卷号: 157, 页码: 189-198
Authors:
Zhong K
;
Yan C
;
Chen SS
;
Wang XY(王小永)
;
Ju SJ
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Adobe PDF(8635Kb)
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View/Download:241/73
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Submit date:2019/05/29
Aeroheating
Heatshield configuration
Sphere-cone angle
Mars
Turbulent