[1] |
Yanhua ZHANG, Dengcheng ZHANG, Zhangwen ZHOU, Yuchang LEI, Lin LI.
Concept and design of virtual rudder surface aircraft based on circulation control: Review
[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 629608-629608.
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[2] |
LI Ni, BU Shuhui, SHANG Bolin, LI Yongbo, TANG Zhili, ZHANG Weiwei.
Aircraft intelligent design: Visions and key technologies
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(4): 524752-524752.
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[3] |
ZHANG Maoquan, CHEN Haixin.
Estimated model of range and endurance of small electric UAVs
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(3): 625085-625085.
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[4] |
HUANG Jun.
Survey on design technology of distributed electric propulsion aircraft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(3): 624037-624037.
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[5] |
LIANG Yu, SHAN Xiaowen.
Aerodynamic analysis and optimization design for variable camber airfoil of civil transport jet
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(3): 790-798.
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[6] |
HAN Zhonghua.
Kriging surrogate model and its application to design optimization: A review of recent progress
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(11): 3197-3225.
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[7] |
SONG Wenbin.
Aero-economics and value-driven aircraft design methodology and applications
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(1): 81-95.
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[8] |
WANG Rong, XIA Pinqi.
Control of Helicopter Rotor Blade Dynamic Stall and Hub Vibration Loads by Multiple Trailing Edge Flaps
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(5): 1083-1091.
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[9] |
ZHANG Shuai, YU Xiongqing.
Sensitivity Analysis of Primary Parameters in Preliminary Design of a Short/Medium-haul Airliner
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(4): 809-816.
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[10] |
Tian Yongliang;Liu Hu;Luo Mingqiang;Wu Zhe.
Research on Case Base of Parameterized Large Civil Aircraft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(11): 2202-2208.
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[11] |
Bai Zhendong;Liu Hu;Xu Min;Wu Zhe.
Preferred Selection Method for Multiobjective Concepts in Aircraft Conceptual Design Optimization
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(8): 1447-1453.
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[12] |
Wang Yu;Yu Xiongqing.
Optimization Method for Aircraft Conceptual Design Under Uncertainty
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(10): 1883-1888.
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[13] |
ZHANG Ke-shi;HAN Zhong-hua;LI Wei-ji;LI Xiang.
Multidisciplinary Aerodynamic/Structural Design Optimization for High Subsonic Transport Wing Using Approximation Technique
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(5): 810-815.
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[14] |
SHI You-jin;ZHANG Zeng-chang.
An Equivalent Multi-mass System of a Flexible Airplane
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(4): 635-640.
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[15] |
WU Jing-min;ZUO Hong-fu.
New Method for Direct Maintenance Cost Estimating by Using CBR
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2005, 26(2): 190-194.
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