[1] |
RAO Chong, ZHANG Tiejun, WEI Chuang, LIU Ying.
Influence mechanism of propeller slipstream on wing of a distributed electric aircraft scheme
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(S1): 726387-726387.
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[2] |
CHEN Yin, GU Yunsong, SUN Zhijun, HUANG Zi.
Aerodynamic perception from distributed pressure and free flight test
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(3): 124138-124138.
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[3] |
LI Runze, ZHANG Yufei, CHEN Haixin.
Strategies and methods for multi-objective aerodynamic optimization design for supercritical wings
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(5): 623409-623409.
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[4] |
HONG Junwu, WANG Yuntao, LI Wei, YANG Xiaochuan.
Numerical simulation of high-lift configuration from HiLiftPW-3
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(3): 122391-122391.
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[5] |
LI Yiqing, HAN Weiqiang, YOU Yancheng, PAN Chengjian.
Integration waverider design of hypersonic inlet and forebody with preassigned pressure distribution
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(9): 2711-2720.
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[6] |
SONG Yanming, YANG Yang.
Numerical Simulation of Hydrostatic Bearing with Self-controlled Restrictor Employing Cooling Roll in Amorphous Alloy Ribbon Formation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(4): 1157-1164.
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[7] |
JING Zhiwei, HOU Zongtuan, GUO Zhaodian.
Flight Loads Design Technique for Flexible Aircraft Airdrop
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(11): 3037-3045.
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[8] |
YANG Kunmiao, ZHANG Weimin, WANG Bin.
Research of Supercritical Wing Optimization Based on Aerodynamic Design Principle of Wing
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(2): 263-272.
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[9] |
LI Qingying, ZHU Chunling, BAI Tian.
Simplification of De-icing Excitation and Influential Factors of the Electro-impulse De-icing System
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(8): 1384-1393.
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[10] |
ZHANG Yufei, CHEN Haixin, FU Song, ZHANG Miao, ZHANG Meihong, LIU Tiejun.
A Practical Optimization Design Method for Transport Aircraft Wing/Nacelle Integration
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(11): 1993-2001.
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[11] |
YANG Chao;XIAO Zhipeng;WAN Zhiqiang.
A Robust Aeroelastic Optimization Method of Structure and Trim for Air Vehicle with Multiple Control Surfaces
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(1): 75-82.
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[12] |
CHEN Shuang;MA Bing-he;YUAN Wei-zheng;JIANG Cheng-yu.
Detection Method of Boundary-Layer Separation Point Based on Micro Pressure Sensor Array
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(4): 574-578.
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[13] |
Liang De-wang;Zhang Shi-ying.
ESTIMATION OF THE MAXIMUM INSTANTANEOUS DISTORTION WITH CORRELATED FLUCTUATION PRESSURES
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1992, 13(7): 427-430.
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[14] |
Zhang Wen-hua;K. Gersten;A. Becker.
CALCULATION OF THE BASE PRESSURE FOR BODY WITH BLUNT-TAIL
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1992, 13(5): 309-312.
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