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1
Prospects of the Aeroengine Control Development in the Early Time of the 21st Century
SUN Jian guo
2001, 16(2): 97-102.
Abstract PDF(163KB) icon11070 icon2017
2
TRANSIENT OPERATING LINE INDICATOR AND ITS APPLICATION
Wang Zongyuan, Fang Jinyan
1986, 1(1): 41-46,91-92.
Abstract PDF(564KB) icon9737 icon1860
3
DEVELOPMENT OF HIGH BY-PASS RATIO TURBOFAN ENGINES
Chen Guang
1986, 1(1): 69-75,94-95.
Abstract PDF(1229KB) icon9564 icon1849
4
EXPERIMENTAL INVESTIGATION ON COMPRESSOR STATOR TANDEM CASCADES AT HIGH SUBSONIC SPEED
Zhuang Biaonan, Guo Bingheng
1986, 1(1): 37-40,91.
Abstract PDF(413KB) icon9380 icon1914
5
AN EXPERIMENTAL STUDY ON A LOBED NOZZLE OF AN INFRARED SUPPRESSION SYSTEM
Zhang Jingzhou, Li Ligao, Gao Chao, He Wenbing
1997, 12(2): 212-214,224.
Abstract PDF(293KB) icon9314 icon1627
6
DOMINANT FACTOR METHOD FOR ANALYZING DYNAMIC BEHAVIOUR OF GAS TURBINE
Ni Weidou, Xu Xiangdong
1986, 1(1): 59-62,93-94.
Abstract PDF(494KB) icon9010 icon1755
7
APPLICATION OF A TWO-DIMENSIONAL LASERDOPPLER ANEMOMETER TO MEASUREMENTIN DIFFUSION FLAME
Ma Jieping, Lin Qixun, Du Qinfang, Xiao Ningfang
1986, 1(1): 27-30,90.
Abstract PDF(469KB) icon8245 icon1842
8
Component-level modeling technology for variable cycle engine
GOU Xue-zhong, ZHOU Wen-xiang, HUANG Jin-quan
2013, 28(1): 104-111.
Abstract PDF(1227KB) icon7540 icon4348
9
The role of AVDR in linear cascade testing
Bo Song, Wing F. Ng
2007, 22(6): 933-944.
Abstract PDF(1067KB) icon7296 icon2250
10
Aero-engine rotor-stator rubbing positions diagnosis rule acquisition based on support vector machine
LI Ai, CHEN Guo, YU Ming-yue
2013, 28(10): 2181-2193.
Abstract PDF(18554KB) icon6615 icon13104
11
Vibration response analysis of gear coupled rotor system considering geometric eccentric effect of helical gears
MA Hui, WANG Qi-bin, HUANG Jing, ZHANG Yi-min
2013, 28(1): 16-24.
Abstract PDF(1409KB) icon6166 icon3779
12
Reaction kinetic numerical simulation of combustion process and emission formation in aero-engine combustor
MA Hong-an, XIE Mao-zhao, ZENG Wen, CHEN Xiao-xiao
2013, 28(2): 297-306.
Abstract PDF(2064KB) icon6138 icon3518
13
Sample points reused failure response curve method for structural reliability analysis
FENG Huan-huan, JIANG Xiang-hua
2013, 28(10): 2228-2234.
Abstract PDF(13073KB) icon5712 icon8697
14
Combustion instability at end of burning in a solid rocket motor
SU Wan-xing, LI Shi-peng, ZHANG Qiao, ZHAO Yan-dong, YE Qing-qing, WANG Ning-fei
2013, 28(10): 2376-2383.
Abstract PDF(11261KB) icon5612 icon6635
15
LOW CYCLE FATIGUE LIFE TESTING RESEARCH OF AN AEROENGINE CASE
Pu Ruigang
1986, 1(1): 11-14,88.
Abstract PDF(397KB) icon5432 icon1524
16
Effect of Knudsen number on microscale similar flow characteristics
XU Yan-zhi, ZHU Hui-ren, ZHENG Jie
2013, 28(8): 1752-1758.
Abstract PDF(991KB) icon5255 icon3859
17
Numerical study on characteristics of temperature reduction and flow loss in radial pre-swirl system
ZHANG Jian-chao, WANG Suo-fang
2013, 28(10): 2284-2291.
Abstract PDF(16307KB) icon5235 icon7042
18
INVESTIGATION ON STEADY-STATE RESPONSE OF ADUAL-ROTOR SYSTEM WITH INTER-SHAETSQUEEZE-FILM DAMPER
Yan Litang, Li Qihan
1986, 1(1): 1-6,87.
Abstract PDF(589KB) icon5207 icon1549
19
Research on aircraft engine component-level models based on GasTurb/MATLAB
ZHANG Shu-gang, GUO Ying-qing, LU Jun
2012, 27(12): 2850-2856.
Abstract PDF(991KB) icon4877 icon1952
20
DIMENSIONLESS PARAMETERS ON ENHANCED HEATTRANSFER IN FLUIDS BY HIGH-FREQUENCYOSCILLATIONS WITHIN PIPES
Zhao Lingde, Cao Yuzhang
1986, 1(1): 21-25,89.
Abstract PDF(420KB) icon4775 icon1480
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