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Knowledge Management System of Institue of Mechanics, CAS
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姜宗林 [2]
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Indexed By:CSCD
Date Issued:2023
Document Type:期刊论文
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Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:
Dai, Chunliang
;
Sun, Bo
;
Yue LJ(岳连捷)
;
Zhou, Shengbing
;
Zhuo, Changfei
;
Zhou, Changsheng
;
Yu, Jianyi
Adobe PDF(5674Kb)
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Submit date:2024/02/19
Scramjet inlet
Starting ability
Thermochemical
Work performance
激波风洞两级入轨飞行器纵向级间分离试验技术
期刊论文
航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126
Authors:
王粤
;
汪运鹏
;
姜宗林
Adobe PDF(6797Kb)
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View/Download:419/44
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Submit date:2022/12/01
两级入轨
轨迹捕获
激波风洞
多体分离
动态试验
试验技术
Decomposition of mean skin friction in incident shock wave/turbulent boundary layer interaction flows at Mach 2.25
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 9, 页码: 178-194
Authors:
Duan JY(段俊亦)
;
Tong FL(童福林)
;
Li XL(李新亮)
;
Liu HW(刘洪伟)
Adobe PDF(6039Kb)
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View/Download:142/11
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Submit date:2023/11/13
Compressible flow
Boundary layers
Direct numerical simulation
Shock waves
Skin friction
Turbulent flow
Method of applying temperature-sensitive paint in hypersonic test with strong combustion radiation
期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 8, 页码: 322474
Authors:
Yuan CK(苑朝凯)
;
Meng FZ(孟凡钊)
;
Liu, Xu
;
Liu YF(刘云峰)
;
Lian H(连欢)
;
Liu, Yingzheng
;
Peng, Di
Adobe PDF(3477Kb)
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Submit date:2023/07/17
Temperature-sensitive paint
Heat flux
Conjugate gradient method
Air-breathing hypersonic vehicle
Inverse heat conduction problem
Linear analysis of the dynamic response of a riser subject to internal solitary waves
期刊论文
APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2023, 卷号: 44, 期号: 6, 页码: 1023-1034
Authors:
Tan, Dalin
;
Wang X(王旭)
;
Duan JL(段金龙)
;
Zhou JF(周济福)
Adobe PDF(280Kb)
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Submit date:2023/07/17
internal solitary wave (ISW)
riser
dynamic response
linear analysis
O352
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
一种并联两级入轨飞行器纵向分离方案的数值研究
期刊论文
航空学报, 2023, 卷号: 44, 期号: 11, 页码: 127634
Authors:
王粤
;
汪运鹏
;
王春
;
姜宗林
Adobe PDF(4901Kb)
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Submit date:2022/07/11
两级入轨
高超声速
纵向分离
气动干扰
非定常流动
A computational method for the load spectra of large-scale structures with a data-driven learning algorithm
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2023, 卷号: 66, 期号: 1, 页码: 141-154
Authors:
Chen XJ(陈贤佳)
;
Yuan, Zheng
;
Li, Qiang
;
Sun, ShouGuang
;
Wei YJ(魏宇杰)
Adobe PDF(2512Kb)
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Submit date:2023/02/09
load spectrum
computational mechanics
deep learning
data-driven modeling
gated recurrent unit neural network
体相微马达双气泡聚并驱动的界面演化机制
期刊论文
物理学报, 2023, 卷号: 72, 期号: 16, 页码: 10.7498/aps.72.20230608
Authors:
王丽娜
;
陈力
;
盛敏佳
;
王雷磊
;
崔海航
;
郑旭
;
黄明华
Adobe PDF(3014Kb)
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Submit date:2023/11/06
dual bubble coalescence
micromotor
interface energy
pseudo potential lattice Boltzmann method
双气泡聚并
微马达
界面能
伪势格子Boltzmann方法