[1] |
WANG Qiang, MA Zhisai, ZHANG Xin, LIU Yan, DING Qian.
Dynamic characteristic analysis for a folding fin with freeplay nonlinearities based on mode synthesis method
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(5): 223507-223507.
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[2] |
WANG Houbing, LIN Guowei, HAN Xuebing, LI Xinxiang.
Shear buckling performance of composite hat-stiffened panels
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(8): 222889-222889.
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[3] |
JIAO Jingpin, LI Haiping, ZHAI Shuncheng, HE Cunfu, WU Bin.
Lamb waves health monitoring technology for metal stiffened plate based on compressive sensing
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(7): 422695-422695.
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[4] |
LIU Guangyuan, ZHANG Lin, CHEN Dehua, LIN Xuedong, JIA Zhiliang.
Experiment on nonlinear flow near perforated wall with slanted holes in transonic wind tunnel
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(5): 122497-122497.
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[5] |
LI Qiang, DONG Guangxu, ZHANG Xinong, LUO Yajun, ZHANG Yahong, XIE Shilin.
Design and parameter optimization of a new tunable dynamic vibration absorber
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(6): 221721-221721.
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[6] |
LI Guojun, BAI Junqiang, TANG Changhong, LIU Nan, QIAO Lei.
Characteristics of laminar separation flutter of two-dimensional airfoils at low Reynolds numbers
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(11): 121280-121280.
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[7] |
GUO Tongbiao, BAI Junqiang, SUN Zhiwei, WANG Chen.
Aeroelastic modeling and analysis of wings considering geometric nonlinearity
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(11): 121351-121351.
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[8] |
MENG Xuanshi, YANG Zeren, CHEN Qi, BAI Peng, HU Haiyang.
Laminar separation control at low Reynolds numbers using plasma actuation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(7): 2112-2122.
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[9] |
YANG Zhichun, TIAN Wei, GU Yingsong, HE Shun.
Advance in the study on wing aeroelasticity with concentrated nonlinearity
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(7): 2013-2044.
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[10] |
DUAN Jingbo, ZHOU Zhou, WANG Wei, JIANG Tao, WANG Rui.
A method for aeroelastic load redistribution of very flexible wing with a high-aspect-ratio
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(3): 799-809.
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[11] |
LI Ruirui, YU Zhihao, YANG Weidong, WU Shen.
A time-domain computational method for dynamic properties and analysis of helicopter rotor elastomeric damper
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(6): 1905-1914.
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[12] |
AN Xiaomin, XU Wei, XU Min.
Analysis of nonlinear panel flutter
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(4): 1119-1127.
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[13] |
SHANG Kun, LIU Xiangyang, LI Meng.
Modeling of spacesuit flat pattern mobility joint based on finite element method
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(3): 1002-1010.
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[14] |
MA Chao, WEI Cheng, ZHAO Yang, WANG Ran.
Modelling method and application of solid beam element based on absolute nodal coordinate formulation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(10): 3316-3326.
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[15] |
WANG Shulei, WEI Ruixuan, GUO Qing, WEI Wenjie.
UAV Guidance Law for Coordinated Standoff Target Tracking
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(6): 1684-1693.
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