[1] |
DU Jianjian, PAN Xiande, LIU Tianyi.
Indirect measurement method for axial load of aero-engine angular contact ball bearing
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 625457-625457.
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[2] |
YANG Te, YANG Zhichun, LIANG Shuya, KANG Zaifei, JIA You.
Feature extraction and identification of stationary random dynamic load using deep neural network
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 225952-225952.
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[3] |
MAO Senxin, SHI Hanyang, LI Kaixiang, ZHANG Xiao, ZHU Yuntao, DU Juan, ZOU Kangzhuang, XIONG Junjiang.
Vibration fatigue load spectrum compilation and test verification
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(7): 426585-426585.
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[4] |
FENG Zhenyu, FU Boyu, XIE Jiang, DUAN Zhuxuan, PAN Hanyuan.
Dynamic response of fuselage panel under explosive impact load
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 525513-525513.
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[5] |
CUI Ming, FENG Jianmin, MI Zheng, GUO Junhao.
Loading technology for main structure of large UAV durability test
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 525887-525887.
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[6] |
LI Chong, CHAI Yanan, WANG Binwen, CHEN Xiangming, YU Zhenbo, ZHOU Hong.
Test technology for complex stress field of large scale fuselage panel
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526409-526409.
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[7] |
ZHANG Tuo, SONG Pengfei, YIN Wei, DU Xing, REN Peng.
Follow-up loading technology for lift structure with spatial complex movement
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526044-526044.
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[8] |
YANG Huan, LIU Xiaochuan, BAI Chunyu, ZHANG Yu, XI Xulong.
Experiment on longitudinal dynamic impact characteristics of typical aircraft seat/occupant system
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526238-526238.
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[9] |
LI Yueming, LI Xiaoyun, CHAI Yijun, YANG Xiongwei.
Dynamic response analysis of nose landing gear in aircraft new towing and taxiing mode
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526915-526915.
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[10] |
GUO Qiong, LIU Wei, PEI Lianjie, GUO Junhao.
Static and fatigue test technology for full-scale composite fuselage barrels
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 525816-525816.
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[11] |
WANG Houbing, WANG Xiahan, LIN Guowei, LI Xinxiang, YANG Shengchun.
Residual strength evaluation of curved hat-stiffened composite panels with discrete-source damage
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 525899-525899.
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[12] |
LI Yueming, LI Xiaoyun, CHAI Yijun, YANG Xiongwei.
Dynamic response analysis of nose landing gear in aircraft new towing and taxiing mode
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526915-526915.
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[13] |
WANG Yupeng, TIAN Wenpeng, SONG Pengfei, XIA Feng, FENG Jianmin.
Research and verification of comprehensive acceleration technology for civil aircraft full-scale fatigue test
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(5): 224919-224919.
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[14] |
YAN Hao, WU Xiaoming.
Topology optimization and structure evolution of turbine disks based on load sensitivity suppression
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(5): 225295-225295.
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[15] |
SU Shaopu, CHANG Wenkui, CHEN Xianmin.
Fatigue buckling test and analytical approach of aircraft typical panel structures
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(5): 225219-225219.
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