| [1] |
Chuanjun CAO, Tianyi LIU, Wei ZHU, Jinchun WANG.
Technology development in high pressure compressor of civil high bypass-ratio turbofan engine
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(12): 27824-027824.
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| [2] |
CAO Ming, HUANG Jinquan, ZHOU Jian, CHEN Xuefeng, LU Feng, WEI Fang.
Current status, challenges and opportunities of civil aero-engine diagnostics & health management Ⅰ: Diagnosis and prognosis of engine gas path, mechanical and FADEC
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 625573-625573.
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| [3] |
PAN Muxuan, CHEN Qianglong, ZHOU Yongquan, ZHOU Wenxiang, HUANG Jinquan.
A multi-dynamics approach to turbofan engine modeling
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(5): 122632-122632.
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| [4] |
TAN Weiwei, YAN Hong, NIE Zhijun, MA Tuliang, LIANG Yihua.
Propulsion performance simulation of turbofan engine for large civil aircraft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(1): 522428-522428.
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| [5] |
ZHANG Yingzhe, NI Daming, Incheol LEE, LIN Dakai, YANG Zhigang.
Test on hot jet noise of scaled engine nozzle
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(12): 122446-122446.
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| [6] |
WANG Zhiqiang, SHEN Xigang, HU Jun.
Prediction and evaluation of aerodynamic stability of high bypass ratio turbofan engine deployed with thrust reverser
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(2): 120192-120202.
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| [7] |
DU Xian, GUO Yingqing, SUN Hao, XU Qingshi.
Sliding mode control based multivariable limit management for aircraft engine
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(12): 3657-3667.
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| [8] |
WU Xinchen, CHEN Minghe, XIE Lansheng, ZHANG Tielei, HU Zhihua.
Twist-bend forming of aeroengine titanium TC4 wide-chord hollow fan blade with complex geometries
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(6): 2055-2063.
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| [9] |
SHAN Yong, ZHANG Jingzhou, SHAO Wanren, WU Fei.
Experimental and Numerical Research on Jet Noise Suppression with Chevron Nozzle for Turbofan Engines
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(5): 1046-1056.
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| [10] |
YOU Jin, XIA Zhixun, FANG Chuanbo, HU Jianxin, LIU Bing.
Study of Starting Characteristics for Mixed-compression Inlet with Instantaneous Injection
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(9): 1590-1598.
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| [11] |
Wang Yi;Fan Xiaoqiang;He Jihong;Chen Ti;Liang Jianhan;Wang Zhenguo.
Effect of Sidewall Geometry on Starting Characteristics of Two-dimensional Hypersonic Inlet
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(2): 217-222.
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| [12] |
LI Ying-hong;LIU Jian-xun.
Turbofan Engine Starting Characteristics Estimation Based on Support Vector Machines
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2005, 26(1): 32-35.
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| [13] |
CHEN Yu-chun;CHEN Bao-yan;LU Yao;ZHANG Jin-liang.
Theoretic and Experimental Research on Cartridge Starting Condition of Turbofan Engine
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2004, 25(2): 121-124.
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