×
验证码:
换一张
Forgotten Password?
Stay signed in
China Science and Technology Network Pass Registration
×
China Science and Technology Network Pass Registration
Log In
Chinese
|
English
中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
Log In
Register
ALL
ORCID
Title
Creator
Thesis Advisor
Keyword
Document Type
Source Publication
Publisher
Date Issued
Date Accessioned
Indexed By
Funding Project
DOI
Study Hall
Image search
Paste the image URL
Home
Collections
Authors
DocType
Subjects
K-Map
News
Search in the results
Collection
State Key... [10]
State Key ... [1]
Creator
李新亮 [10]
童福林 [4]
reprint au... [2]
Chen XP [1]
Zhu ZC [1]
于剑 [1]
More...
Document Type
Journal a... [10]
Date Issued
2023 [1]
2021 [1]
2020 [2]
2019 [2]
2017 [1]
2013 [2]
More...
Language
英语 [7]
中文 [3]
Source Publication
CHINESE JO... [3]
ACTA MECHA... [1]
Chinese Ph... [1]
SCIENCE CH... [1]
SCIENCE CH... [1]
力学学报 [1]
More...
Indexed By
CSCD [10]
EI [9]
SCI [7]
Funding Project
National N... [2]
LHD Youth ... [1]
National K... [1]
National K... [1]
National K... [1]
National N... [1]
More...
Funding Organization
National K... [2]
National N... [2]
LHD Youth ... [1]
National B... [1]
National K... [1]
National N... [1]
More...
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
(Note: the search results are based on claimed items)
Browse/Search Results:
1-10 of 10
Help
Filters
Indexed By:CSCD
Creator:李新亮
First author
Author:李新亮
Selected(
0
)
Clear
Items/Page:
5
10
15
20
25
30
35
40
45
50
55
60
65
70
75
80
85
90
95
100
Sort:
Select
Journal Impact Factor Ascending
Journal Impact Factor Descending
Submit date Ascending
Submit date Descending
Title Ascending
Title Descending
WOS Cited Times Ascending
WOS Cited Times Descending
Issue Date Ascending
Issue Date Descending
Author Ascending
Author Descending
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)
  |  
Favorite
  |  
View/Download:125/9
  |  
Submit date:2023/11/13
Compressible flow
Boundary layers
Direct numerical simulation
Shock waves
Skin friction
Turbulent flow
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)
  |  
Favorite
  |  
View/Download:223/55
  |  
Submit date:2021/06/07
Direct numerical simulation
Low-frequency unsteadiness
Shock waves
Turbulent boundary layer
Wavy-wall
Subgrid-scale model based on the vorticity gradient tensor for rotating turbulent flows
期刊论文
ACTA MECHANICA SINICA, 2020, 页码: 9
Authors:
Qi H(齐涵)
;
Li XL(李新亮)
;
Yu ZP(于长平)
Adobe PDF(2084Kb)
  |  
Favorite
  |  
View/Download:368/85
  |  
Submit date:2020/07/06
Large-eddy simulation
Subgrid-scale model
Rotating turbulent channel flow
基于十亿亿次国产超算系统的流体力学软件众核适应性研究
期刊论文
计算机科学, 2020, 卷号: 47, 期号: 1, 页码: 24-30
Authors:
李芳
;
李志辉
;
徐金秀
;
范昊
;
褚学森
;
李新亮
Adobe PDF(824Kb)
  |  
Favorite
  |  
View/Download:317/74
  |  
Submit date:2019/12/16
国产
众核架构
流体力学软件
适应性
编程语言
并行算法
超声速膨胀角入射激波/湍流边界层干扰直接数值模拟研究
期刊论文
航空学报, 2019, 页码: 21
Authors:
童福林
;
孙东
;
袁先旭
;
李新亮
Adobe PDF(1603Kb)
  |  
Favorite
  |  
View/Download:204/70
  |  
Submit date:2019/12/16
激波/湍流边界层干扰
膨胀角
本征正交分解
直接数值模拟
Effects of dimensional wall temperature on velocity-temperature correlations in supersonic turbulent channel flow of thermally perfect gas
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2019, 卷号: 62, 期号: 6, 页码: AR64711
Authors:
Chen XP
;
Li XL(李新亮)
;
Zhu ZC
Adobe PDF(1844Kb)
  |  
Favorite
  |  
View/Download:328/102
  |  
Submit date:2019/04/11
direct numerical simulation
velocity-temperature correlation
supersonic flow
channel flow
thermally perfect gas
strong Reynolds analogy
激波与转捩边界层干扰非定常特性数值分析
期刊论文
力学学报, 2017, 卷号: 49, 期号: 01, 页码: 93-104
Authors:
童福林
;
李新亮
;
唐志共
Adobe PDF(23333Kb)
  |  
Favorite
  |  
View/Download:280/58
  |  
Submit date:2017/12/22
激波/边界层干扰
转捩
低频振荡
低通滤波
直接数值模拟
Improvement of Baldwin-Lomax turbulence model for supersonic complex flows
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 3, 页码: 529–534
Authors:
Zhao R(赵瑞)
;
Yan C(阎超)
;
Yu J(于剑)
;
Li XL(李新亮)
;
Yan, C (reprint author), Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China.
Adobe PDF(1609Kb)
  |  
Favorite
  |  
View/Download:895/296
  |  
Submit date:2013/09/21
Baldwin-lomax Model
Boundary Layers
Computational Aerodynamics
Entropy
Supersonic Flows
Turbulence Models
Direct Numerical Simulation of Chemical Non-equilibrium Turbulent Flow
期刊论文
Chinese Physics Letters, 2013, 卷号: 30, 期号: 6, 页码: 064702/1-064702/5
Authors:
Chen XP(陈小平)
;
Li XL(李新亮)
;
Li, XL (reprint author), Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(922Kb)
  |  
Favorite
  |  
View/Download:872/377
  |  
Submit date:2013/09/21
Channel Flows
Turbulent Flows
Non-equilibrium Turbulent Flow
Chemical Reactions
Direct Numerical Simulation
Direct Numerical Simulation of Shock/Turbulent Boundary Layer Interaction in a Supersonic Compression Ramp
期刊论文
SCIENCE CHINA: Physics, Mechanics & Astronomy, 2010, 卷号: 53, 期号: 9, 页码: 1651-1658
Authors:
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Liang X(梁贤)
;
Li XL(李新亮)
Adobe PDF(951Kb)
  |  
Favorite
  |  
View/Download:1616/368
  |  
Submit date:2010/10/25
compression Ramp
Shock/turbulent Boundary Layer Interaction
Direct Numerical Simulation
Shock Oscillation