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Gas Turbine Experiment and Research
1672-2620
2007 Issue 3
Open Rotor Engine, the Power for Next Generation of B737/A320?
HU Xiao-yu
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page:61-62
Redesign of a High Speed Micro-centrifugal Compressor
YIN Ming-xia;GUI Xing-min
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page:57-60
Study on Fatigue-creep Properties of DD6 NI-based Single Crystal Superalloy
QING Hua;JIANG He-fu;WEN Wei-dong;WU Chang-bo;HU Ren-gao;QIN Zhi-xian;SUN Jing-guo
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page:51-56
Compilation of Aeroengine Three Cycle Spectrum
PENG Jing-bo;XIE Shou-sheng;LENG Min;WANG Yun-sheng
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page:48-50,33
Experimental Research on the Harmonic Oil Whip in Sliding Bearing-rotor System
YANG Jin-fu;YANG Kun;FU Zhong-guang;YANG Sheng-bo;YU Da-ren;CUI Ying;ZHANG Zhan-yi
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page:42-47
Experimental Investigation of Temperature Measurement on the Wall of an Afterburner
JI He-ming;WANG Nai-xu;SHAO Wan-ren
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page:39-41
Parametric (On-design) Analysis for a Separate-exhaust Turbofan Engine with Interstage Turbine Burner
PAN Xu;GE Ning
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page:34-38
Corner Separation Control by Bleed Slot at the Root of Blade
MU Xiao-qiang;LU Li-peng
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page:28-33
Base Pressure Influence on the Trailing Edge Loss of Transonic Turbine Cascade
JIANG Zheng-li;LING Dai-jun
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page:23-27
Aerodynamic Design of Fan/Compressor Operated at Low Reynolds Number
GUI Xing-min;LI Xiao-juan
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page:18-22
Research and Experiment on FGH96 P/M Superalloy Sub-scale Disk
CAO Feng-lan;QING Hua;GU Yuan-xing;WU Chang-bo;ZHOU Quan
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page:15-17,27
Effect of Number of Critical Features on Disk LCF Life
WANG Wei-guo;QING Hua;DU Wen-jun
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page:11-14
Design Analysis for Compound Cooling of High Temperature Rise Combustor Wall & Head Shield
LI Bin;CHENG Bo
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page:8-10,56
Constructing and Developing of Aeroengine Design System
WANG Yong-ming;WEI Gang;LAN Fa-xiang;HUANG Shun-zhou
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page:1-7