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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 [14]
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Indexed By:CSCD
Creator:姜宗林
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Document Type:期刊论文
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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)
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Submit date:2021/03/03
Hypersonics
Shock tunnels
Flow characteristics
高超声速喷管设计理论与方法
期刊论文
力学进展, 2020, 卷号: 51, 期号: 02, 页码: 257-294
Authors:
汪运鹏
;
姜宗林
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Submit date:2021/01/29
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)
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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
Simulation of shear layers interaction and unsteady evolution under different double backward-facing steps
期刊论文
Theoretical and Applied Mechanics Letters, 2020, 卷号: 10, 页码: 224-229
Authors:
Deng F(邓芳)
;
Han GL(韩桂来)
;
Jiang ZL(姜宗林)
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Submit date:2021/06/11
Interaction
Jet
Numerical simulation
Shear layer
Unsteady evolution
Shock/shock interactions between bodies and wings
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 2, 页码: 255-261
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Teng HH(腾宏辉)
;
Jiang ZL(姜宗林)
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Submit date:2018/10/30
Body And Wing
Flow Field
Hypersonic Flow
Shock/shock Interaction
Wave Configurations
超声速三维进气道内激波干扰的研究
期刊论文
推进技术, 2017, 期号: 12, 页码: 6
Authors:
项高翔
;
王春
;
汪运鹏
;
姜宗林
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View/Download:485/102
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Submit date:2017/12/22
高超声速流动
箱式进气道
侧壁压缩进气道
波系结构
流场区域
超高速流动模拟及热化学反应模型对比研究
期刊论文
北京航空航天大学学报, 2017, 卷号: 43, 期号: 06, 页码: 1173-1181
Authors:
周凯
;
李旭东
;
胡宗民
;
姜宗林
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Submit date:2017/12/22
超高速
膨胀管
数值模拟
热化学反应模型
适用范围
Theories and technologies for duplicating hypersonic flight conditions for ground testing
期刊论文
NATIONAL SCIENCE REVIEW, 2017, 卷号: 4, 期号: 3, 页码: 290-U461
Authors:
Jiang ZL(姜宗林)
;
Yu HR(俞鸿儒)
;
Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing, Peoples R China.
;
Jiang, ZL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing, Peoples R China.
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Submit date:2017/11/29
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