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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
2016 [4]
2012 [4]
2000 [1]
学科主题
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Numerical Study of Improving Aerodynamic Performance of Low Solidity LPT Cascade through Increasing Trailing Edge Thickness
期刊论文
OAI收割
2016
作者:
Li, C., Yan, P. G., Wang, X. F., Han, W. J. and Wang, Q. C.
收藏
  |  
浏览/下载:45/0
  |  
提交时间:2017/05/27
Aircraft engine low pressure turbine trailing edge thickness profile loss flow control vortex-generator jets separation control local variables
Combined Experimental and Numerical Investigations on the Roughness Effects on the Aerodynamic Performances of LPT Blades
期刊论文
OAI收割
2016
作者:
Berrino, M., Bigoni, F., Simoni, D., Giovannini, M., Marconcini, M., Pacciani, R. and Bertini, F.
收藏
  |  
浏览/下载:37/0
  |  
提交时间:2017/05/27
low-pressure turbine high-load profile roughness unsteady inflow CFD turbulence model transition separation Thermodynamics Engineering
Numerical Study of Combining Steady Vortex Generator Jets and Deflected Trailing Edge to Reduce the Blade Numbers of Low Pressure Turbine Stage
期刊论文
OAI收割
2016
作者:
Li, C., Yan, P. G., Wang, X. F., Han, W. J. and Wang, Q. C.
收藏
  |  
浏览/下载:30/0
  |  
提交时间:2017/05/27
low pressure turbine
profile loss
flow control
Vortex Generator Jets
deflected trailing edge
separation control
local variables
part i transition
Experimental Analysis of the Aerodynamic Performance of an Innovative Low Pressure Turbine Rotor
期刊论文
OAI收割
2016
作者:
Infantino, D., Satta, F., Simoni, D., Ubaldi, M., Zunino, P. and Bertini, F.
收藏
  |  
浏览/下载:26/0
  |  
提交时间:2017/05/27
Low Pressure Turbine
Single Stage Research Turbine
Rotor Aerodynamic
Loading Hot-wire Anemometry
blade row interaction
flow-field
axial gaps
stage
Effects of Freestream Turbulence on Bypass Transition of Separated Boundary Layer on Low-Pressure Turbine Airfoils
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2012, 卷号: 21, 期号: 3, 页码: 230,235
Hideo Taniguchi
;
Hiroshi Sakai
;
Ken-ichi Funazaki
收藏
  |  
浏览/下载:14/0
  |  
提交时间:2013/01/07
Aeroengine
Low-Pressure Turbine
Bypass Transition
Separation Bubble
Unsteady Inflow Effects on the Wake Shed from a High-Lift LPT Blade Subjected to Boundary Layer Laminar Separation
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2012, 卷号: 21, 期号: 2, 页码: 97,108
Francesca Satta
;
Marina Ubaldi
;
Pietro Zunino
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2013/01/07
Wake-wake unsteady interaction
high-lift blade profiles
low-pressure turbine blade wake
A Method for the Determination of Turbulence Intensity by Means of a Fast Response Pressure Probe and its Application in a LP Turbine
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2012, 卷号: 21, 期号: 1, 页码: 21,31
Davide Lengani
;
Berardo Paradiso
;
Andreas Marn
收藏
  |  
浏览/下载:15/0
  |  
提交时间:2013/01/07
Turbulence
fast response aerodynamic pressure probe
low pressure turbine.
Unsteady Inflow Effects on the Wake Shed from a High-Lift LPT Blade Subjected to Boundary Layer Laminar Separation
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2012, 卷号: 21, 期号: 2, 页码: 97,108
作者:
Francesca Satta
;
Marina Ubaldi
;
Pietro Zunino
  |  
收藏
  |  
浏览/下载:26/0
  |  
提交时间:2013/01/07
Wake-wake Unsteady Interaction
High-lift Blade Profiles
Low-pressure Turbine Blade Wake
Control of LP Turbine Rotor Blade Underloading Using Stator Blade Compound Lean at Root
期刊论文
OAI收割
JOURNAL OF THERMAL SCIENCE, 2000, 卷号: 9, 期号: 2, 页码: 115,121
Piotr Lampart
收藏
  |  
浏览/下载:18/0
  |  
提交时间:2013/03/12
axial turbine
low-pressure stage
stage losses
separation
shock wave
compound lean