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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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State Key ... [8]
力学所知识产出(19... [1]
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姜宗林 [9]
王春 [9]
项高翔 [4]
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Creator:王春
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Language:英语
Document Type:期刊论文
Author:姜宗林
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Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle
期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
Adobe PDF(5479Kb)
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Submit date:2022/08/24
Multistage Launch Vehicle
Aerodynamic Characteristics
Shock Wave Interaction
Angle of Attack
Waverider
Boundary Layer Flow
Total Variation Diminishing
Adverse Pressure Gradient
Hypersonic Flows
Hypersonic Wind Tunnels
Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing
期刊论文
AIAA JOURNAL, 2021, 页码: 12
Authors:
Lin MY(林明月)
;
Wang C(王春)
;
Peng J(彭俊)
;
Jiang ZL(姜宗林)
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Submit date:2022/01/12
Three-dimensional shock wave configurations induced by two asymmetrical intersecting wedges in supersonic flow
期刊论文
SHOCK WAVES, 2018, 卷号: 28, 期号: 2, 页码: 311-319
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Teng HH(腾宏辉)
;
Jiang ZL(姜宗林)
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View/Download:565/149
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Submit date:2018/10/30
Supersonic Flow
3d Shock/shock Interaction
3d Asymmetrical Wave Configurations
Spatial Dimension Reduction
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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View/Download:320/76
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Submit date:2018/10/30
Body And Wing
Flow Field
Hypersonic Flow
Shock/shock Interaction
Wave Configurations
Investigations of Three-Dimensional Shock/Shock Interactions over Symmetrical Intersecting Wedges
期刊论文
AIAA JOURNAL, 2016, 卷号: 54, 期号: 5, 页码: 1472-1481
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2016/09/14
Ceramics
Thermal Shock
Size Effect
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
On the numerical technique for the simulation of hypervelocity test flows
期刊论文
Computers & Fluids, 2015, 卷号: 106, 页码: 12-18
Authors:
Hu ZM(胡宗民)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
;
Khoo BC
;
Hu ZM(胡宗民)
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Submit date:2014/11/27
Hypervelocity Test Flow
Dcd Scheme
Flux-splitting
Spurious Oscillation
Analytical and numerical investigations of the reflection of asymmetric nonstationary shock waves
期刊论文
SHOCK WAVES, 2012, 卷号: 22, 期号: 5, 页码: 435-449
Authors:
Yang Y(杨旸)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
;
Yang, Y
;
Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2013/01/18
Asymmetric Shock Waves
Mach Reflection
Detachment Criterion
Mach Reflection
Transition
Boundaries
Domains
Gas
Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows
期刊论文
SHOCK WAVES, 2008, 卷号: 18, 期号: 1, 页码: 41-51
Authors:
Hu ZM(胡宗民)
;
Myong R S
;
Wang C(王春)
;
Cho T H
;
Jiang ZL(姜宗林)
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Submit date:2020/08/26
Shock
Shock Interaction
Oscillation
Hypersonic
Double-wedge
Numerical Study