×
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 ... [8]
Creator
李进平 [8]
陈宏 [8]
张晓源 [4]
俞鸿儒 [3]
岳连捷 [3]
张仕忠 [3]
More...
Document Type
Journal ar... [8]
Date Issued
2022 [2]
2021 [1]
2020 [2]
2019 [1]
2018 [1]
2012 [1]
More...
Language
中文 [4]
英语 [4]
Source Publication
力学学报 [3]
APPLIED SC... [1]
INTERNATIO... [1]
SENSORS [1]
Shock Wave... [1]
爆炸与冲击 [1]
More...
Indexed By
EI [6]
CSCD [4]
SCI [4]
Funding Project
National N... [2]
China Scho... [1]
National N... [1]
National N... [1]
National N... [1]
National N... [1]
More...
Funding Organization
National N... [3]
China Scho... [1]
Youth Inno... [1]
中国科学院“关键技术... [1]
国家自然科学基金(1... [1]
国家自然科学基金资助... [1]
More...
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
Browse/Search Results:
1-8 of 8
Help
Filters
Creator:李进平
First author
Creator:陈宏
Document Type:期刊论文
Community:高温气体动力学国家重点实验室
First author affiliation
The first author
Corresponding 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
Issue Date Ascending
Issue Date Descending
Submit date Ascending
Submit date Descending
Journal Impact Factor Ascending
Journal Impact Factor Descending
WOS Cited Times Ascending
WOS Cited Times Descending
Title Ascending
Title Descending
Author Ascending
Author Descending
高马赫数燃烧强化的激波风洞试验研究
期刊论文
力学学报, 2022, 卷号: 54, 期号: 05, 页码: 1403-1413
Authors:
张旭
;
张启帆
;
岳连捷
;
孟东东
;
罗苇航
;
于江鹏
;
张晓源
;
李进平
;
陈宏
;
李飞
Adobe PDF(3069Kb)
  |  
Favorite
  |  
View/Download:272/53
  |  
Submit date:2022/08/11
高马赫数
超声速燃烧
燃烧强化
小支板
JF-24激波风洞
高马赫数超燃冲压发动机技术研究进展
期刊论文
力学学报, 2022, 卷号: 54, 期号: 02, 页码: 263-288
Authors:
岳连捷
;
张旭
;
张启帆
;
陈科挺
;
李进平
;
陈昊
;
姚卫
;
仲峰泉
;
李飞
;
王春
;
陈宏
Adobe PDF(2622Kb)
  |  
Favorite
  |  
View/Download:580/110
  |  
Submit date:2022/03/16
高马赫数
超燃冲压发动机
热化学非平衡
超声速燃烧
低雷诺数流动
激波风洞
飞行试验
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors:
Zhou GX(周功喜)
;
Zhang X(张旭)
;
Li JP(李进平)
;
Zhang XY(张晓源)
;
Zhang SZ(张仕忠)
;
Lin X(林鑫)
;
Li F(李飞)
;
Chen H(陈宏)
;
Yue LJ(岳连捷)
;
Yu XL(余西龙)
Adobe PDF(4108Kb)
  |  
Favorite
  |  
View/Download:345/54
  |  
Submit date:2021/09/07
High mach number scramjet
Circular cross-section
TDLAS
Multi-view simultaneous imaging
POD
A Fast-Response Calorimeter with Dynamic Corrections for Transient Heat Transfer Measurements
期刊论文
APPLIED SCIENCES-BASEL, 2020, 卷号: 10, 期号: 17, 页码: 22
Authors:
Zhang SZ(张仕忠)
;
Wang Q(汪球)
;
Li JP(李进平)
;
Zhang XY(张晓源)
;
Chen H(陈宏)
Adobe PDF(8566Kb)
  |  
Favorite
  |  
View/Download:212/52
  |  
Submit date:2020/11/30
calorimeter
shock tunnel
heat transfer measurement
hypersonic
Coaxial Thermocouples for Heat Transfer Measurements in Long-Duration High Enthalpy Flows
期刊论文
SENSORS, 2020, 卷号: 20, 期号: 18, 页码: 18
Authors:
Zhang SZ(张仕忠)
;
Wang Q(汪球)
;
Li JP(李进平)
;
Zhang XY(张晓源)
;
Chen H(陈宏)
Adobe PDF(7131Kb)
  |  
Favorite
  |  
View/Download:312/94
  |  
Submit date:2020/11/30
heat transfer measurement
coaxial thermocouple
long-duration
semi-infinite
high enthalpy
用于爆轰驱动的射流起爆实验研究
期刊论文
爆炸与冲击, 2019, 卷号: 39, 期号: 06, 页码: 13-22
Authors:
陆星宇
;
李进平
;
陈宏
;
俞鸿儒
View
  |  
Adobe PDF(1287Kb)
  |  
Favorite
  |  
View/Download:326/66
  |  
Submit date:2019/09/12
爆轰
湍流射流
起爆
激波风洞
爆轰驱动
高超声速溢流冷却实验研究
期刊论文
力学学报, 2018, 卷号: 50, 期号: 1, 页码: 1-8
Authors:
苑朝凯
;
李进平
;
陈宏
;
姜宗林
;
俞鸿儒
View
  |  
Adobe PDF(570Kb)
  |  
Favorite
  |  
View/Download:420/98
  |  
Submit date:2018/10/24
高超声速热防护
主动冷却
溢流冷却
液膜
A chemical shock tube driven by detonation
期刊论文
Shock Waves, 2012, 卷号: 22, 期号: 4, 页码: 351-362
Authors:
Li JP(李进平)
;
Chen H(陈宏)
;
Yu HR(俞鸿儒)
;
Li, J
;
Chinese Acad Sci, Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(848Kb)
  |  
Favorite
  |  
View/Download:825/274
  |  
Submit date:2013/01/18
Shock Tube
Detonation Driver
Chemical Kinetics Study