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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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Key Labora... [3]
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姜宗林 [3]
刘云峰 [2]
孙振旭 [2]
杨国伟 [2]
王梦莹 [2]
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Date Issued:2021
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Effect of surface roughness on the aerodynamics of a high-speed train subjected to crosswinds
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
Authors:
Wang MY(王梦莹)
;
Hashmi, S. A.
;
Sun ZX(孙振旭)
;
Guo DL(郭迪龙)
;
Vita, G.
;
Yang GW(杨国伟)
;
Hemida, H.
Adobe PDF(2683Kb)
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View/Download:330/72
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Submit date:2021/08/16
High-speed train
Surface roughness
Crosswinds
Aerodynamics
Flow separation
Experimental and numerical investigations into flow features in an intake duct for the waterjet propulsion under mooring conditions
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 18
Authors:
Huang RF(黄仁芳)
;
Zhang, Ruizhi
;
Wang YW(王一伟)
;
Luo, Xianwu
;
Zhu, Lei
Adobe PDF(11187Kb)
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View/Download:256/54
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Submit date:2021/06/21
Waterjet propulsion
Particle image velocimetry (PIV)
Intake duct
Waterjet pump
Mooring conditions
Aerodynamic shape optimization of an urban maglev train
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 16
Authors:
Sun ZX(孙振旭)
;
Wang MY(王梦莹)
;
Wei LY(魏涟漪)
;
Kong FB
;
Yang GW(杨国伟)
Adobe PDF(2376Kb)
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View/Download:322/84
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Submit date:2021/06/15
Urban maglev train
Aerodynamic characteristics
Cross validation
Kriging model
Genetic algorithm
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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View/Download:295/65
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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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View/Download:422/74
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Submit date:2021/03/03
Hypersonics
Shock tunnels
Flow characteristics