×
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... [21]
Creator
张新宇 [21]
仲峰泉 [10]
岳连捷 [6]
reprint au... [5]
邢云绯 [4]
余西龙 [3]
More...
Document Type
Conferenc... [13]
Journal ar... [8]
Date Issued
2015 [21]
Language
中文 [15]
英语 [6]
Source Publication
第八届全国高超声速科... [7]
中国力学大会-201... [4]
20th AIAA ... [1]
ACTA MECHA... [1]
AEROSPACE ... [1]
APPLIED TH... [1]
More...
Indexed By
EI [8]
CSCD [5]
SCI [5]
Funding Project
Funding Organization
National N... [1]
National N... [1]
Natural Sc... [1]
This work ... [1]
This work ... [1]
国家自然科学基金(9... [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 21
Help
Filters
Date Issued:2015
Author:张新宇
First author
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
Author Ascending
Author Descending
WOS Cited Times Ascending
WOS Cited Times Descending
Title Ascending
Title Descending
Issue Date Ascending
Issue Date Descending
Submit date Ascending
Submit date Descending
Journal Impact Factor Ascending
Journal Impact Factor Descending
Numerical study of combustion and convective heat transfer of a Mach 2.5 supersonic combustor
期刊论文
APPLIED THERMAL ENGINEERING, 2015, 卷号: 89, 页码: 883-896
Authors:
Wang X
;
Zhong FQ(仲峰泉)
;
Gu HB(顾宏斌)
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
Adobe PDF(4711Kb)
  |  
Favorite
  |  
View/Download:286/125
  |  
Submit date:2016/01/08
Supersonic Combustor
Convective Heat Transfer
Numerical Study
Wall Heat Flux
Development of efficient and accurate skeletal mechanisms for hydrocarbon fuels and kerosene surrogate
期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 5, 页码: 732-740
Authors:
Zhong FQ(仲峰泉)
;
Ma SG
;
Zhang XY(张新宇)
;
Sung CJ
;
Niemeyer KE
;
Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(1318Kb)
  |  
Favorite
  |  
View/Download:281/88
  |  
Submit date:2016/01/08
Reduced Chemistry
Hydrocarbons
Directed Relation Graph
Ignition Delay Time
Numerical study of heat transfer deterioration of turbulent supercritical kerosene flow in heated circular tube
期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2015, 卷号: 85, 页码: 1003-1011
Authors:
Dang GX
;
Zhong FQ(仲峰泉)
;
Zhang YJ
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Bei Si Huan Xi Rd 15, Beijing 100190, Peoples R China.
Adobe PDF(2856Kb)
  |  
Favorite
  |  
View/Download:453/132
  |  
Submit date:2015/06/12
Supercritical Kerosene
Convective Heat Transfer
Turbulent Flow
Numerical Study
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
Authors:
Wang ZP(王知溥)
;
Li F(李飞)
;
Gu HS
;
Yu XL(余西龙)
;
Zhang XY(张新宇)
;
Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1112Kb)
  |  
Favorite
  |  
View/Download:531/223
  |  
Submit date:2015/06/12
Scramjet
Dual-mode Combustor
Divergent Angle
Cavity Location
Combustion Efficiency
Tdlas
双模态发动机的模态鉴别方法
期刊论文
力学学报, 2015, 期号: 3, 页码: 389-397
Authors:
李飞
;
王知溥
;
余西龙
;
顾洪斌
;
陈立红
;
张新宇
Adobe PDF(3140Kb)
  |  
Favorite
  |  
View/Download:423/74
  |  
Submit date:2015/12/25
双模态冲压发动机
模态鉴别
释热分布
H_2O/CO_2污染对RP-3航空煤油着火特性的影响
期刊论文
推进技术, 2015, 卷号: 36, 期号: 3, 页码: 336-344
Authors:
梁金虎
;
王苏
;
张灿
;
张胜涛
;
岳连捷
;
范秉诚
;
张新宇
;
崔季平
Adobe PDF(1583Kb)
  |  
Favorite
  |  
View/Download:230/61
  |  
Submit date:2015/12/25
污染效应
着火延时
煤油
H2o
Co2
激波管
Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel
期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 3, 页码: 470-475
Authors:
Xing YF(邢云绯)
;
Zhong FQ(仲峰泉)
;
Li DX(李东霞)
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(860Kb)
  |  
Favorite
  |  
View/Download:433/184
  |  
Submit date:2015/04/28
Hypersonic Scramjet Test Tunnel
Nozzle
Aerodynamic Heating
Convective Heat Transfer
用于超燃诊断的吸收光谱二维诊断技术
会议论文
北京力学会第21届学术年会暨北京振动工程学会第22届学术年会, 中国北京, 2015-01-11
Authors:
李飞
;
余西龙
;
曾徽
;
张少华
;
顾洪斌
;
张新宇
Adobe PDF(737Kb)
  |  
Favorite
  |  
View/Download:596/176
  |  
Submit date:2015/05/14
可调谐二极管吸收光谱技术(Tdlas)
二维断层成像术(Tdlat)
温度分布
高超声速进气道快速破膜开启的流动特性
期刊论文
航空学报, 2015, 卷号: 36, 期号: 6, 页码: 1795-1804
Authors:
徐骁
;
岳连捷
;
卢洪波
;
肖雅彬
;
张新宇
Adobe PDF(711Kb)
  |  
Favorite
  |  
View/Download:290/61
  |  
Submit date:2015/12/25
高超声速进气道
破膜开启
非定常效应
激波边界层相互作用
分离流
Large eddy simulation of ignition and combustion of ethylene/air turbulent jet diffusion flame with reduced kinetic mechanism
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Ma SG(马素刚)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Zhong, Fengquan (fzhong@imech.ac.cn)
Adobe PDF(496Kb)
  |  
Favorite
  |  
View/Download:240/71
  |  
Submit date:2017/05/05
Combustion Pro
Cess
Directed Relation Graph
Dynamic Evolution
Fuel Injection Velocities
Kinetic Mechanism
Reduced Mechanisms
Temperature Profiles
Temporal And Spatial Evolutions