×
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... [15]
力学所知识产出(19... [3]
Creator
张新宇 [18]
李飞 [12]
余西龙 [10]
陈立红 [9]
reprint au... [7]
顾洪斌 [6]
More...
Document Type
Journal a... [11]
Conference... [7]
Date Issued
2019 [1]
2017 [1]
2015 [2]
2014 [2]
2013 [4]
2012 [1]
More...
Language
英语 [16]
中文 [2]
Source Publication
AEROSPACE ... [2]
力学学报 [2]
15th AIAA ... [1]
16th AIAA/... [1]
17th AIAA ... [1]
21st AIAA ... [1]
More...
Indexed By
EI [18]
SCI [9]
CSCD [4]
CPCI-S [1]
Funding Project
National N... [1]
Youth Inno... [1]
Funding Organization
American I... [1]
National N... [1]
National N... [1]
National S... [1]
Natural Sc... [1]
The projec... [1]
More...
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
Browse/Search Results:
1-10 of 18
Help
Filters
Indexed By:EI
Creator:zhangxinyu分张新宇
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
WOS Cited Times Ascending
WOS Cited Times Descending
Issue Date Ascending
Issue Date Descending
Author Ascending
Author Descending
Submit date Ascending
Submit date Descending
Title Ascending
Title Descending
Journal Impact Factor Ascending
Journal Impact Factor Descending
Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
Authors:
Fan WH(范文慧)
;
Zhong FQ(仲峰泉)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
Adobe PDF(4075Kb)
  |  
Favorite
  |  
View/Download:307/90
  |  
Submit date:2020/03/11
Wall heat flux
Numerical simulation
Ethylene
Supersonic combustor
Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Cheng LW(程柳维)
;
Zhong FQ(仲峰泉)
;
Wang ZP(王知溥)
;
Gu HB(顾洪斌)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
Adobe PDF(517Kb)
  |  
Favorite
  |  
View/Download:328/107
  |  
Submit date:2018/01/16
Combustors
Cracks
Diesel Engines
Efficiency
Ethylene
Fighter Aircraft
Fuels
High Speed Cameras
Ignition
Kerosene
Luminance
Spacecraft
Stabilization
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.
View
  |  
Adobe PDF(4711Kb)
  |  
Favorite
  |  
View/Download:309/134
  |  
Submit date:2016/01/08
Supersonic Combustor
Convective Heat Transfer
Numerical Study
Wall Heat Flux
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.
View
  |  
Adobe PDF(1112Kb)
  |  
Favorite
  |  
View/Download:552/229
  |  
Submit date:2015/06/12
Scramjet
Dual-mode Combustor
Divergent Angle
Cavity Location
Combustion Efficiency
Tdlas
The vitiation effects of water vapor and carbon dioxide on the autoignition characteristics of kerosene
期刊论文
Acta Mechanica Sinica, 2014, 卷号: 30, 期号: 4, 页码: 485-494
Authors:
Liang JH(梁金虎)
;
Wang S(王苏)
;
Zhang ST(张胜涛)
;
Yue LJ(岳连捷)
;
Fan BC(范秉诚)
;
Zhang XY(张新宇)
;
Cui JP(崔季平)
;
Wang S(王苏)
View
  |  
Adobe PDF(1351Kb)
  |  
Favorite
  |  
View/Download:889/218
  |  
Submit date:2014/08/14
Ignition Delay
Vitiation Effect
Kerosene
Water
Carbon Dioxide
Shock Tube
基于CN自由基的火星再入流场温度测量
期刊论文
力学学报, 2014, 卷号: 46, 期号: 2, 页码: 201-208
Authors:
林鑫
;
余西龙
;
李飞
;
张少华
;
辛建国
;
张新宇
View
  |  
Adobe PDF(818Kb)
  |  
Favorite
  |  
View/Download:420/130
  |  
Submit date:2014/11/05
发射光谱
谱线强度
火星再入
转动温度
振动温度
Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 卷号: 28, 期号: 1, 页码: 72-78
Authors:
Li F(李飞)
;
Yu XL(余西龙)
;
Tong YG(仝颖刚)
;
Shen Y(沈岩)
;
Chen J(陈健)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View
  |  
Adobe PDF(1235Kb)
  |  
Favorite
  |  
View/Download:1325/420
  |  
Submit date:2013/07/30
Scramjet
Kerosene Fuel
Plasma Torch
Ignition
Numerical simulation of ignition and combustion of ethylene in a supersonic model combustor with a reduced kinetic mechanism
期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2013, 卷号: 185, 期号: 4, 页码: 548-563
Authors:
Zhong FQ(仲峰泉)
;
Chen LH(陈立红)
;
Li F(李飞)
;
Zhang XY(张新宇)
;
Sung CJ
;
Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(1454Kb)
  |  
Favorite
  |  
View/Download:1429/487
  |  
Submit date:2013/05/03
Ethylene
Ignition
Numerical Simulation
Reduced Kinetic Mechanism
Supersonic Combustion
CO concentration and temperature measurements in a shock tube for Martian mixtures by coupling OES and TDLAS
期刊论文
APPLIED PHYSICS B-LASERS AND OPTICS, 2013, 卷号: 110, 期号: 3, 页码: 401-409
Authors:
Lin X(林鑫)
;
Yu XL(余西龙)
;
Li F(李飞)
;
Zhang SH(张少华)
;
Xin JG
;
Zhang XY(张新宇)
;
Yu XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(716Kb)
  |  
Favorite
  |  
View/Download:1078/338
  |  
Submit date:2013/04/16
Diode-laser Absorption
Nonequilibrium Radiation
Cn Radiation
Sensor
Entry
Flows
Wave
Combined TDLAS and OES technique for CO concentration measurement in shock-heated Martian atmosphere
会议论文
2nd International Symposium on Laser Interaction with Matter (LIMIS), Xian, PEOPLES R CHINA, SEP 09-12, 2012
Authors:
Lin X(林鑫)
;
Yu XL(余西龙)
;
Li F(李飞)
;
Zhang SH(张少华)
;
Xin JG
;
Zhang XY(张新宇)
;
Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View
  |  
Adobe PDF(683Kb)
  |  
Favorite
  |  
View/Download:807/281
  |  
Submit date:2013/12/12
Optical Emission Spectroscopy (Oes)
Tunable Diode Laser Absorption Spectroscopy (Tdlas)
Shock Wave
Temperature
Concentration