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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 [3]
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Indexed By:SCI
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Computational study of lateral jet interaction in hypersonic thermochemical non-equilibrium flows using nonlinear coupled constitutive relations
期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 11, 页码: 14
Authors:
Zeng, Shuhua
;
Yang, Junyuan
;
Zhao, Wenwen
;
Huang YF(黄依峰)
;
Jiang, Zhongzheng
;
Chen, Weifang
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Submit date:2024/01/22
Numerical Study on the Aerodynamic Heating Characteristics of the Cantilevered Injection System for Oblique Detonation Engine Inlets
期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 10, 页码: 18
Authors:
Yang F(杨帆)
;
Lin MY(林明月)
;
Hu ZM(胡宗民)
;
Han GL(韩桂来)
Adobe PDF(8946Kb)
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Submit date:2023/11/28
oblique detonation engine
cantilevered injection
localized high heat flux
boundary layer separation
reattachment
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)
Adobe PDF(4805Kb)
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Submit date:2022/01/12
Fluid-structure interaction-based aerodynamic modeling for flight dynamics simulation of parafoil system
期刊论文
NONLINEAR DYNAMICS, 2021, 页码: 22
Authors:
Zhu, Hong
;
Sun, Qinglin
;
Liu, Xuefeng
;
Liu, Jinglei
;
Sun, Hao
;
Wu WN(邬婉楠)
;
Tan, Panlong
;
Chen, Zengqiang
Adobe PDF(4213Kb)
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Submit date:2021/08/03
Fluid-structure interaction
Parafoil system
Flexible deformation
Trailing edge deflection
Aerodynamic performance
Dynamic model
Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
Authors:
Tong FL(童福林)
;
Sun D(孙栋)
;
Li XL(李新亮)
Adobe PDF(4402Kb)
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View/Download:216/51
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Submit date:2021/06/07
Direct numerical simulation
Low-frequency unsteadiness
Shock waves
Turbulent boundary layer
Wavy-wall
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
Impulse force-measurement system
期刊论文
SHOCK WAVES, 2020, 页码: 11
Authors:
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(1551Kb)
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Submit date:2020/11/30
Shock tunnel
High enthalpy
Aerodynamic force measurement
Strain gauge balance
Characterizing three-dimensional features of vortex surfaces in the flow past a finite plate
期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 1, 页码: 15
Authors:
Tong WW
;
Yang Y(杨越)
;
Wang SZ(王士召)
Adobe PDF(6216Kb)
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Submit date:2020/05/18
External-Compression Supersonic Inlet Free from Violent Buzz
期刊论文
AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523
Authors:
Chen H
;
Tan H
;
Liu YZ
;
Zhang QF(张启帆)
Adobe PDF(4679Kb)
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Submit date:2019/09/09
Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules
期刊论文
ACTA ASTRONAUTICA, 2019, 卷号: 157, 页码: 189-198
Authors:
Zhong K
;
Yan C
;
Chen SS
;
Wang XY(王小永)
;
Ju SJ
Adobe PDF(8635Kb)
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View/Download:233/73
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Submit date:2019/05/29
Aeroheating
Heatshield configuration
Sphere-cone angle
Mars
Turbulent