[1] |
SUN Canfei, HUANG Linran, SHEN Yong.
Fault diagnosis of helicopter planetary gear transmission system under complex operating conditions
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 625480-625480.
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[2] |
YANG Zongyao, ZHANG Jingzhou, SHAN Yong.
Effects of slot-inlet arrangement at infrared-suppressor-integrated rear airframe on flow organization and infrared radiation characteristics
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 124445-124445.
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[3] |
CHEN Yaping, YU Jianjian, HU Lei, WANG Yutang.
Characteristics and application of bending moments of helicopter rotor shaft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524168-524168.
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[4] |
LI Yanqing, XUAN Yimin.
Coupling analysis method for helicopter thermal management and infrared radiation characteristics
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(3): 124270-124270.
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[5] |
WANG Luofeng, CHEN Renliang.
Rigid-elastic coupled flight dynamic modeling and air resonance stability analysis for heavy lift helicopter
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(12): 124634-124634.
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[6] |
HU Zhou, WANG Zhisheng, WANG Congqing.
Decoupling Control Algorithm of Helicopter with Input Saturation Based on Information Fusion
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(5): 1394-1403.
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[7] |
LIU Yang, XIANG Jinwu.
Effect of the Trailing Edge Flap on Dynamic Stall Performance of Helicopter Rotor Airfoil
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(5): 1028-1035.
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[8] |
WANG Bo, ZHAO Qijun, ZHAO Guoqing, XU Guohua.
Experimental Research and Numerical Analysis on Aerodynamic Characteristics of Rotors with Improved CLOR Blade-tip
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(2): 235-245.
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[9] |
QI Xuewen, YAN Jian'gang, YANG Dawei, GAO Dongfei.
Study on Subsets of Searching Region Division Models of Coordinated Anti-submarine by Helicopters
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(11): 2599-2606.
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[10] |
PAN Chengxiong;ZHANG Jingzhou;SHAN Yong.
Modeling and Analysis of Helicopter Skin Temperature Distribution
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(2): 249-256.
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[11] |
SONG Laishou, XIA Pinqi.
Coupled Fuselage/Piezoelectric Stack Actuator Optimization Method for Active Vibration Control of Helicopter
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(10): 1835-1841.
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[12] |
Yang Jianling;Zhang Liyan;Zhou Shaohua;Fang Yonghong;Huang Wenjun.
Geometric Modeling of Composite Helicopter Rotor Blade Plies
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(1): 191-197.
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[13] |
Yang Yidong;Yuan Weidong.
HELICOPTER VIBRATION REDUCTION TECHNIQUE WITH HARMONIC ACTIVE CONTROL
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(5): 55-60.
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[14] |
Wang Zili.
INVESTIGATION OF RELIABILITY AND MAINTAINABILITY PARAMETERS FOR HELICOPTERS
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1995, 16(S1): 20-27.
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[15] |
Cao Yihua.
OPERATION REQUIREMENTS OF TURRETED GUN IN HELICOPTER AIR COMBAT AND MATHEMATIC INVERSE SOLUTION
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1995, 16(3): 22-29.
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