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高超声速尖锥边界层转捩实验研究
期刊论文
空天技术, 2023, 期号: 03, 页码: 1-14
Authors:
刘美宽
;
韩桂来
;
李宗贤
;
姜宗林
Adobe PDF(3144Kb)
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View/Download:112/42
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Submit date:2023/08/02
高超声速
边界层转捩
大尺度模型
风洞实验
不稳定波
高超声速边界层液膜演化过程和冷却机理研究
期刊论文
力学学报, 2023, 页码: 15
Authors:
骆寅涛
;
韩桂来
;
钱丽娟
;
姜宗林
;
刘美宽
Adobe PDF(2195Kb)
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View/Download:160/71
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Submit date:2023/05/08
高超声速
液膜冷却
液膜演化
壁面热流
VOF
Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 96-106
Authors:
Peng J(彭俊)
;
Li S(李帅)
;
Yang F(杨帆)
;
Lin MY(林明月)
;
Han GL(韩桂来)
;
Hu ZM(胡宗民)
Adobe PDF(2838Kb)
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Submit date:2023/04/20
Shock interactions
Transitional configuration
Aerodynamic heating
Shear layer
Mach interaction
Hypersonic shock wave and turbulent boundary layer interaction in a sharp cone/flare model
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 80-95
Authors:
Tong FL(童福林)
;
Duan JY(段俊亦)
;
Lai, Jiang
;
Sun, Dong
;
Yuan, Xianxu
Adobe PDF(4757Kb)
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Submit date:2023/04/20
Shock wave
Hypersonic turbulent
boundary layer
Heat transfer
Skin friction decomposition
Direct numerical simulation
不同飞行高度下超声速来流/射流及其相互作用的数值模拟
期刊论文
上海大学学报(自然科学版), 2021, 卷号: 27, 期号: 02, 页码: 307-324
Authors:
邓放
;
韩桂来
;
刘美宽
;
丁珏
;
翁培奋
;
姜宗林
Adobe PDF(2690Kb)
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Submit date:2021/08/25
后台阶
射流
剪切层
数值模拟
JF-12激波风洞在火星进入环境下的运行特性
期刊论文
航空学报, 2021, 卷号: 42, 期号: 03, 页码: 189-200
Authors:
韩子健
;
彭俊
;
胡宗民
;
韩桂来
;
姜宗林
Adobe PDF(5070Kb)
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View/Download:369/94
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Submit date:2021/04/19
火星探测
反向爆轰驱动激波风洞
二氧化碳
缝合运行状态
驻室压力
Noise reduction for temperature-sensitive paint measurement contaminated by strong background radiation in a high enthalpy hypersonic tunnel
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 7
Authors:
Peng, Di
;
Liu, Xu
;
Jiao, Lingrui
;
Li, Ziyan
;
Wen, Xin
;
Yuan CK(苑朝凯)
;
Han GL(韩桂来)
;
Liu YF(刘云峰)
;
Liu, Yingzheng
;
Jiang ZL(姜宗林)
Adobe PDF(3477Kb)
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Submit date:2021/03/30
Temperature-sensitive paint
Time-resolved measurement
Hypersonic flow
Background radiation
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
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)
Adobe PDF(1546Kb)
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Submit date:2021/06/11
Interaction
Jet
Numerical simulation
Shear layer
Unsteady evolution
Aerodynamic measurement of a large aircraft model in hypersonic flow
期刊论文
CHINESE PHYSICS B, 2017, 卷号: 26, 期号: 11, 页码: 114702-1-114702-6
Authors:
Meng BQ(孟宝清)
;
Han GL(韩桂来)
;
Zhang DL(张德良)
;
Jiang ZL(姜宗林)
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Submit date:2017/12/18
Hypersonic
Aerodynamic Measurement
Theoretical Study
Vibration