中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
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CAS IR Grid
机构
工程热物理研究所 [9]
采集方式
OAI收割 [9]
内容类型
期刊论文 [9]
发表日期
2010 [4]
2003 [5]
学科主题
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The Effect of Diffuser Angle on the Discharge Coefficient of a Miniature Critical Nozzle
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2010, 卷号: 19, 期号: 3, 页码: 222,227
Jae Hyung Kim1
;
Heuy Dong Kiml*
;
Toshiaki Setoguchi2
收藏
  |  
浏览/下载:17/0
  |  
提交时间:2013/01/06
Compressible Flow
Critical Nozzle
Compressible Flow
Discharge Coefficient
Diffuser Configuration
Reynolds Number
Experimental Study on the Inlet Fogging System Using Two-Fluid Nozzles
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2010, 卷号: 19, 期号: 2, 页码: 132,135
Abhilash Suryan1
;
Dong Sun Kim2
;
Heuy Dong Kiml
收藏
  |  
浏览/下载:15/0
  |  
提交时间:2013/01/31
Evaporative Cooling
Inlet Fogging
Energy Savings
Two-fluid Nozzles
The Effect of Diffuser Angle on the Discharge Coefficient of a Miniature Critical Nozzle
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2010, 卷号: 19, 期号: 3, 页码: 222,227
作者:
Heuy Dong Kiml*
;
Toshiaki Setoguchi2
;
Jae Hyung Kim1
  |  
收藏
  |  
浏览/下载:17/0
  |  
提交时间:2013/01/06
Compressible Flow
Critical Nozzle
Compressible Flow
Discharge Coefficient
Diffuser Configuration
Reynolds Number
Experimental Study on the Inlet Fogging System Using Two-Fluid Nozzles
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2010, 卷号: 19, 期号: 2, 页码: 132,135
作者:
Abhilash Suryan1
;
Dong Sun Kim2
;
Heuy Dong Kiml
  |  
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2013/01/31
Evaporative Cooling
Inlet Fogging
Energy Savings
Two-fluid Nozzles
A Study of the Vortical Flow over a Delta Wing with a Leading Edge Extension
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2003, 卷号: 12, 期号: 4, 页码: 299,303
Heuy-Dong Kiml
;
Young-Ki Leel
;
Tae-Ho Kiml
;
Myoung-Hwan Sohn2
收藏
  |  
浏览/下载:15/0
  |  
提交时间:2013/03/12
delta wing
leading edge extension (LEX)
vortex core
vortex strength.
A Study of the Impulse Wave Discharged from the Exits of Two Parallel Tubes
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2003, 卷号: 12, 期号: 4, 页码: 332,336
Yong-Hun Kweon1
;
Heuy-Dong Kiml
;
Toshiaki Setoguchi2
;
Toshiyuki Aoki3
收藏
  |  
浏览/下载:18/0
  |  
提交时间:2013/03/12
compressible flow
unsteady flow
impulse wave
shock wave
shock tube.
Study for the Gas Flow through a Critical Nozzle
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2003, 卷号: 12, 期号: 3, 页码: 250,254
Jae-Hyung Kiml
;
Heuy-Dong Kiml
;
Shigeru Matsuo
;
Toshiaki Setoguchi
收藏
  |  
浏览/下载:19/0
  |  
提交时间:2013/03/12
compressible flow
choke
boundary layer
critical pressure ratio
discharge coefficient.
A Study of the Vortical Flow over a Delta Wing with a Leading Edge Extension
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2003, 卷号: 12, 期号: 4, 页码: 299,303
作者:
Heuy-Dong Kiml
;
Young-Ki Leel
;
Tae-Ho Kiml
;
Myoung-Hwan Sohn2
  |  
收藏
  |  
浏览/下载:20/0
  |  
提交时间:2013/03/12
Delta Wing
Leading Edge Extension (Lex)
Vortex Core
Vortex Strength.
A Study of the Impulse Wave Discharged from the Exits of Two Parallel Tubes
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2003, 卷号: 12, 期号: 4, 页码: 332,336
作者:
Yong-Hun Kweon1
;
Heuy-Dong Kiml
;
Toshiaki Setoguchi2
;
Toshiyuki Aoki3
  |  
收藏
  |  
浏览/下载:23/0
  |  
提交时间:2013/03/12
Compressible Flow
Unsteady Flow
Impulse Wave
Shock Wave
Shock Tube.