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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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胡宗民 [7]
姜宗林 [5]
刘云峰 [2]
张子健 [2]
李进平 [2]
汪运鹏 [2]
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Funding Organization:National Natural Science Foundation of China
Author:胡宗民
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Community:高温气体动力学国家重点实验室
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Study on aerodynamic loads at the inlet's cowl lip induced by multiple shock-shock interferences
期刊论文
ACTA MECHANICA SINICA, 2024, 卷号: 40, 期号: 4, 页码: 12
Authors:
Lin MY(林明月)
;
Yang F(杨帆)
;
Hu ZM(胡宗民)
;
Han GL(韩桂来)
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View/Download:14/0
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Submit date:2024/05/27
Shock waves
Shock-shock interaction
Theoretical analysis
Hysteresis
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:349/177
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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
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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View/Download:271/101
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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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View/Download:258/60
  |  
Submit date:2020/07/06
Effects of boundary layer on wedge-induced oblique detonation structures in hydrogen-air mixtures
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2019, 卷号: 44, 期号: 41, 页码: 23429-23435
Authors:
Fang YS(方宜申)
;
Zhang ZJ(张子健)
;
Hu ZM(胡宗民)
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Adobe PDF(1085Kb)
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View/Download:283/91
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Submit date:2019/10/21
Oblique detonation wave
Boundary layer
Viscosity
Detonation initiation
Hydrogen-air mixture
Weighting by Cross-Validation: A Calibration Method for Force Measurements via Transient Response Analysis
期刊论文
EXPERIMENTAL TECHNIQUES, 2019, 卷号: 43, 期号: 4, 页码: 469-478
Authors:
Luo ZT(罗长童)
;
Wang YP(汪运鹏)
;
Hu ZM(胡宗民)
;
Li JP(李进平)
;
Jiang ZL(姜宗林)
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Adobe PDF(2227Kb)
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View/Download:279/67
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Submit date:2019/10/21
Aerodynamic force measurement
Dynamic system
Impact response
Cross-validation
System identification
A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
Authors:
Peng J(彭俊)
;
Zhang ZJ(张子健)
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
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Adobe PDF(2165Kb)
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View/Download:416/96
  |  
Submit date:2019/09/09
Shock reflection
Vibration excitation
Mach reflection
Transition criterion
Hypersonic flow