×
验证码:
换一张
忘记密码?
记住我
CORC
首页
科研机构
检索
知识图谱
申请加入
托管服务
登录
注册
在结果中检索
科研机构
力学研究所 [5]
清华大学 [2]
北京大学 [1]
工程热物理研究所 [1]
内容类型
期刊论文 [8]
会议论文 [1]
发表日期
2023 [1]
2022 [2]
2016 [1]
2015 [1]
2010 [2]
2006 [1]
更多...
×
知识图谱
CORC
开始提交
已提交作品
待认领作品
已认领作品
未提交全文
收藏管理
QQ客服
官方微博
反馈留言
浏览/检索结果:
共9条,第1-9条
帮助
已选(
0
)
清除
条数/页:
5
10
15
20
25
30
35
40
45
50
55
60
65
70
75
80
85
90
95
100
排序方式:
请选择
发表日期升序
发表日期降序
提交时间升序
提交时间降序
题名升序
题名降序
作者升序
作者降序
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
作者:
Dai, Chunliang
;
Sun, Bo
;
Yue LJ(岳连捷)
;
Zhou, Shengbing
;
Zhuo, Changfei
收藏
  |  
浏览/下载:1/0
  |  
提交时间:2024/02/19
Scramjet inlet
Starting ability
Thermochemical
Work performance
Lagrange Optimization of Shock Waves for Two-Dimensional Hypersonic Inlet with Geometric Constraints
期刊论文
AEROSPACE, 2022, 卷号: 9, 期号: 10, 页码: 15
作者:
Li YL(李育凌)
;
Yue LJ(岳连捷)
;
He CM(何成明)
;
Wu WN(邬婉楠)
;
Chen H(陈昊)
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2022/11/14
scramjet inlet
Lagrange optimization method
shock configuration
Influence of high temperature non-equilibrium effects on Mach 12 scramjet inlet
期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 193, 页码: 237-254
作者:
Dai, Chunliang
;
Sun, Bo
;
Zhou, Shengbing
;
Zhuo, Changfei
;
Zhou, Changsheng
收藏
  |  
浏览/下载:34/0
  |  
提交时间:2022/05/17
Mach 12 scramjet inlet
High temperature
Non-equilibrium effects
Thermochemical
Inlet performance
Design methodology for shape transition inlets based on constant contraction of discrete streamtubes
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 卷号: 230, 期号: 8, 页码: 1496-1506
作者:
Xiao YB(肖雅斌)
;
Yue LJ(岳连捷)
;
Ma SH
;
Zhang XY(张新宇)
收藏
  |  
浏览/下载:26/0
  |  
提交时间:2016/09/14
Hypersonic inlet
shape transition
inward turning
scramjet
design method
Classification of Combustor-Inlet Interactions for Airbreathing Ramjet Propulsion
期刊论文
AIAA JOURNAL, 2015
Cui, Tao
;
Wang, Yong
;
Liu, Kai
;
Jin, Jianren
收藏
  |  
浏览/下载:5/0
  |  
提交时间:2017/12/03
TRANSONIC DIFFUSER FLOW
MODE TRANSITION
HYSTERESIS PHENOMENON
SCRAMJET ENGINES
SUPERSONIC INLET
SHOCK POSITION
UNSTART
OSCILLATIONS
DYNAMICS
SIMULATION
Design and optimization of inlet performance based on hybrid genetic algorithm
期刊论文
2010, 2010
Zhou Jian-xing
;
Piao Ying
;
Cao Zhi-song
收藏
  |  
浏览/下载:6/0
基于混合遗传算法的进气道性能设计与优化
期刊论文
2010, 2010
周建兴
;
朴英
;
曹志松
;
ZHOU Jian-xing
;
PIAO Ying
;
CAO Zhi-song
收藏
  |  
浏览/下载:1/0
Research on three-dimensional scramiet inlet
会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
作者:
Yue LJ(岳连捷)
;
Chen LH(陈立红)
;
Xiao YB
;
Gong P
;
Chang XY(张新宇)
收藏
  |  
浏览/下载:8/0
  |  
提交时间:2017/06/01
Capture ratio
Mass flow
Surface oil dot visualization
Three-dimensional scramjet inlet
The Two-Dimensional Supersonic Flow and Mixing with a Perpendicular Injection in a Scramjet Combustor
期刊论文
JOURNAL OF THERMAL SCIENCE, 2003, 卷号: 12, 期号: 4, 页码: 371,380
Mohammad Ali
;
S. Ahmed
;
A.K.M. Sadrul Islam
收藏
  |  
浏览/下载:11/0
  |  
提交时间:2013/03/12
scramjet engine
TVD scheme
finite width of inlet
supersonic mixing
parallel air stream
flame holding.
©版权所有 ©2017 CSpace - Powered by
CSpace