Home
|
Survey
|
Payment
|
Talks & Presentations
|
Job Opportunities
Journals
A
B
C
D
E
F
G
H
I
J
K
L
M
N
O
P
Q
R
S
T
U
V
W
X
Y
Z
Gas Turbine Experiment and Research
1672-2620
2009 Issue 3
Numerical Study of Two Dimensional Flow on an Oscillating Airfoil
ZHANG Zheng-qiu;ZOU Zheng-ping;LIU Huo-xing
..............
page:1-8
Aerodynamic Performance Validation of P&W E3 High Pressure Turbine Stage
XIANG Chuan-guo;WANG Bin;QING Xiong-jie
..............
page:9-13
3D Computational Study of Axisymmetric Dual-throat Fluidic Thrust-vectoring Nozzles
QING Tai-mu;LIAO Hua-lin;ZHU Chuan
..............
page:14-18
Effects of Turbine Tip Clearance on Gas Turbine Performance
ZHAO Wang-dong;ZHOU Yu-bin;YANG Rui
..............
page:19-22,44
Research on Low Cycle Fatigue Life of a Compressor Disc
DU Wen-jun;WANG Wei-guo;HE Min;MENG Ling-yong
..............
page:23-27
Research on Fracture of Compressor Blade Dovetail from Fretting Wear
DUAN Jia-kuan;YANG Xing-yu;DONG Li-wei;WANG Bing
..............
page:28-32
Research on Identification Modeling for Control System Based on SVR
WANG Wen-dong;GUO Wei
..............
page:33-36
Investigation on Correction Methods of Aero-engine Components Characteristics Based on Model Identification
BAI Lei;CHEN Si-bing;JIANG He-fu
..............
page:37-39,13
Heat Transfer Experimental Investigation on Full Film Cooling of Turbine Vane Surface
LIANG Wei-ying;ZHOU Lei-sheng
..............
page:40-44
Experimental Investigation of Flow Characteristics in Pre-swirl Nozzles
LIU Bo;WANG Yong-hong
..............
page:45-46,62
Preliminary Analysis of the Windage Temperature Rise in Rotating Labyrinth Seals
HU Yan-li;LIU Yu-fang;WANG Peng-fei
..............
page:47-49
Application of Exergy Efficiency in Gas Path Fault of Gas Turbine
HE Xing;SUN Feng-rui;ZHOU Mi;LIU Yong-bao;YU You-hong
..............
page:50-53,59
Research on the Application of Laser Shock Processing Technology on Aero-engine Blade
HU Ya-ji;CHEN Yan-chu;CHEN Dong
..............
page:54-56
Analysis of Technique for "Lift Thrust" Aircraft
ZHOU Ren-zhi;PENG Shi;HOU Yong-jin
..............
page:57-59
Open Rotor Engine is Hopeful to Power the Next Generation A320/B737 after 2020
HU Xiao-yu
..............
page:60-62