[1] |
Fanmin MENG, Nuo MA, Wenchao MA, Junhui MENG, Wenguang LI.
Wet modal analysis and tests for inflatable wing with swept air-beams
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 227098-227098.
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[2] |
ZHANG Xingyu, GAO Zhenghong, LEI Tao, MIN Zhihao, LI Weiling, ZHANG Xiaobin.
Ground test on aerodynamic-propulsion coupling characteristics of distributed electric propulsion aircraft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 125389-125389.
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[3] |
LIU Xiaochuan, LIU Chongchong, MOU Rangke.
Research progress on shimmy dynamics of aircraft landing gear systems
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 527063-527063.
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[4] |
TANG Xiaofeng, HE Zhenwei, CHANG Hongzhen, SHI Xiaoming, PAN Qiang, TANG Guoan.
Thermo-modal test on an axle bearing supported rudder and identification of its supporting stiffness
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(6): 222617-222617.
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[5] |
TANG Xiaofeng, CHANG Hongzhen, HE Zhenwei, SHI Xiaoming, TANG Guoan.
Thermo-modal test and simulation of spindly vehicle in free boundary conditions
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(10): 222095-222095.
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[6] |
DOU Qingbo, YANG Zhichun, LIU Xiaochuan, MU Rangke, YANG Hai.
Test method for full scale drop of carrier-based aircraft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(3): 220421-220421.
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[7] |
WU Dafang, WANG Yuewu, SHANG Lan, PU Ying, WANG Huaitao.
Test research and numerical simulation on thermal modal of plate structure in 1200℃ high-temperature environments
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(6): 1861-1875.
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[8] |
LIU Hao, LI Xiaodong, YANG Wenqi, SUN Xiasheng.
Thermal vibration test on wing structure of high-speed flight vehicle using TARMA model method
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(7): 2225-2235.
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[9] |
LUO Wukui, TAN Shen'gang, XIE Huaiqiang, HUO Yingyuan.
Research on Methods Used to Determine Flutter Model Design Factors
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(10): 2383-2390.
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[10] |
FU Zhichao, ZHONG Weiguo, CHEN Zhiping, ZHU Zhenyu, LV Ji'nan, LIU Ziqiang, JIA Yongqing.
Experimental Study on Structural Dynamic Characteristics of Flexible High-aspect-ratio Wings
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(9): 2177-2184.
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[11] |
WU Dafang, ZHAO Shougen, PAN Bing, WANG Yuewu, MU Meng, WU Shuang.
Research on Thermal-vibration Joint Test for Wing Structure of High-speed Cruise Missile
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(9): 1633-1642.
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[12] |
FENG Fei, CHANG Zheng, NIE Hong, ZHANG Ming, PENG Yiming.
Analysis of Influence of Aircraft Flexibility on Nose Landing Gear Shimmy
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(12): 2227-2235.
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[13] |
Cui Xuli;Chen Huaihai;He Xudong;You Weiqian.
PID Control with Variable Arguments for MIMO Random Vibration Test
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(9): 1776-1780.
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[14] |
Yang Hui;He Li;Wang Yanrong.
Experimental Study on Aeroelasticity in Linear Oscillating Compressor Cascade. PartⅡ: Tipclearance Effect
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2008, 29(4): 804-810.
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[15] |
Yang Hui;He Li;Wang Yanrong.
Experimental Study on Aeroelasticity in Linear Oscillating Compressor Cascade. PartⅠ: Unsteady Aerodynamic Response
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2008, 29(4): 795-803.
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