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姜宗林 [26]
胡宗民 [26]
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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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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
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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Submit date:2019/09/09
Shock reflection
Vibration excitation
Mach reflection
Transition criterion
Hypersonic flow
Hypervelocity Test with a Detonation-Driven Expansion Tube
会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:
Hu ZM(胡宗民)
;
Zhou K(周凯)
;
Peng J(彭峻)
;
Jiang ZL(姜宗林)
Adobe PDF(297Kb)
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Submit date:2020/01/06
Spectral measurements of hypervelocity flow in an expansion tunnel
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
Authors:
Yuan CK(苑朝凯)
;
Zhou K(周凯)
;
Liu YF(刘云峰)
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
Adobe PDF(1468Kb)
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Submit date:2019/04/11
Spectral measurement
Hypervelocity flow
Radiation
Expansion tunnel
Starting Process in a Large-Scale Shock Tunnel
期刊论文
AIAA Journal, 2016, 卷号: 54, 期号: 5, 页码: 1240-1249
Authors:
Wang YP(汪运鹏)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
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Submit date:2017/09/19
Theoretical solutions to three-dimensional asymmetrical shock/shock interaction
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 8, 页码: 1208-1216
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Hu ZM(胡宗民)
;
Li XD
;
Jiang ZL(姜宗林)
;
Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
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Submit date:2016/12/08
3d Asymmetrical Shock/shock Interaction
Spatial-dimension Reduction
Mach Reflection
Flow Field
Theoretical Analysis
Starting Process in a Large-Scale Shock Tunnel
会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
Authors:
Wang YP
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Wang, YP (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2016/06/28
Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel
会议论文
22nd AIAA Computational Fluid Dynamics Conference, 2015, Dallas, TX, United states, June 22, 2015 - June 26, 2015
Authors:
Wang YP(汪运鹏)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
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Submit date:2017/05/05
Inviscid Flows
Numerical Investigations
Outlet Diameters
Reflected Shock Waves
Simulated Results
Starting Process
Transmitted Shock
Unsteady Nozzle Flow
超高速流动研究进展
会议论文
中国力学大会——2013, 中国北京, 2013-08-19
Authors:
胡宗民
;
姜宗林
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View/Download:495/158
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Submit date:2014/04/02
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