×
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 ... [9]
宽域飞行工程科学与应... [2]
微重力重点实验室 [1]
Creator
姜宗林 [2]
崔凯 [2]
常思源 [2]
张凯凯 [2]
李广利 [2]
汪运鹏 [2]
More...
Document Type
Journal a... [10]
Date Issued
2023 [10]
Language
中文 [5]
英语 [5]
Source Publication
航空学报 [4]
CHINESE JO... [3]
ACTA MECHA... [2]
力学学报 [1]
Indexed By
CSCD [10]
EI [10]
SCI [5]
Funding Project
China Post... [1]
China Scho... [1]
Foundation... [1]
Fundamenta... [1]
National K... [1]
Opening Fo... [1]
More...
Funding Organization
中国科学院基础前沿科... [2]
国家自然科学基金(1... [2]
China Post... [1]
China Scho... [1]
Foundation... [1]
Fundamenta... [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 10
Help
Filters
Indexed By:CSCD
Date Issued:2023
Document Type:期刊论文
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
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)
  |  
Favorite
  |  
View/Download:67/10
  |  
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)
  |  
Favorite
  |  
View/Download:408/42
  |  
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
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)
  |  
Favorite
  |  
View/Download:61/7
  |  
Submit date:2023/07/17
Temperature-sensitive paint
Heat flux
Conjugate gradient method
Air-breathing hypersonic vehicle
Inverse heat conduction problem
翼反角对高压捕获翼构型高超气动特性的影响
期刊论文
航空学报, 2023, 卷号: 44, 期号: 08, 页码: 45-58
Authors:
常思源
;
肖尧
;
李广利
;
田中伟
;
张凯凯
;
崔凯
Adobe PDF(3584Kb)
  |  
Favorite
  |  
View/Download:200/41
  |  
Submit date:2022/10/17
高压捕获翼
高超声速
数值模拟
上/下反角
稳定性
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)
  |  
Favorite
  |  
View/Download:63/3
  |  
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)
  |  
Favorite
  |  
View/Download:53/2
  |  
Submit date:2023/04/20
Shock wave
Hypersonic turbulent
boundary layer
Heat transfer
Skin friction decomposition
Direct numerical simulation
机体尾缘形状对高压捕获翼构型亚声速特性影响
期刊论文
航空学报, 2023, 卷号: 44, 期号: 06, 页码: 10.7527/S1000-6893.2022.27215
Authors:
王浩祥
;
肖尧
;
张凯凯
;
李广利
;
常思源
;
田中伟
;
崔凯
Adobe PDF(2111Kb)
  |  
Favorite
  |  
View/Download:191/52
  |  
Submit date:2022/10/17
高压捕获翼
亚声速
流动特性
流动分离
数值模拟
On the accuracy of two temperature models for hypersonic nonequilibrium flow
期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 2, 页码: 122193
Authors:
Wang XY(王小永)
;
Hong QZ(洪启臻)
;
Hu Y(胡远)
;
Sun QH(孙泉华)
Adobe PDF(2067Kb)
  |  
Favorite
  |  
View/Download:65/3
  |  
Submit date:2023/04/20
Nonequilibrium flow
Two temperature model
Quasi classical trajectory
Non Boltzmann effect
Vibration dissociation coupling effect
高速弹丸诱导斜爆轰激波结构实验研究
期刊论文
力学学报, 2023, 卷号: 55, 期号: 02, 页码: 309-317
Authors:
尚甲豪
;
胡国暾
;
汪球
;
王业军
;
张坤
;
项高翔
;
赵伟
;
魏炳忱
Adobe PDF(1612Kb)
  |  
Favorite
  |  
View/Download:240/59
  |  
Submit date:2023/03/16
斜爆轰
超声速燃烧
激波诱导燃烧
斜爆轰波
二级轻气炮
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)
  |  
Favorite
  |  
View/Download:611/92
  |  
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