[1] |
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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[2] |
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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[3] |
LI Yuhai, WANG Chengbo, CHEN Liang, DONG Hongda, GUAN Yu, DI Hongliang, GU Yuxuan.
Overview on development of advanced fighter life design and extension technology
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525791-525791.
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[4] |
CHEN Yaping, YU Jianjian, HU Lei, WANG Yutang.
Characteristics and application of bending moments of helicopter rotor shaft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524168-524168.
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[5] |
QI Xiaofeng, YANG Yu, KANG Weiping, WANG Qian.
Fatigue damage monitoring of lug joints with random load spectrum based on acoustic emission
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524518-524518.
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[6] |
MIN Qiang, WANG Bintuan, WANG Yafang, LEI Xiaoxin.
Compiling load spectrum method for arrested deck-landing of carrier-based aircraft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(4): 622284-622284.
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[7] |
LEI Xiaoxin, ZHANG Yanjun, JI Luming, ZHU Liang.
Equivalent analysis spectrum construction method for aircraft structure containing cracks
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(S1): 721577-721577.
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[8] |
HE Xiaofan, DONG Yinghao, LI Yuhai, LIU Wenting.
Probabilistic fracture mechanics approach accounting for both the variability of load spectra and of structural properties
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(4): 1142-1149.
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[9] |
BAI Xin, XIE Liyang.
Fatigue Crack Growth Law Prediction Based on Steady Random Load
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(9): 2500-2505.
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[10] |
HE Xiaofan, WANG Qiang, LIU Wenting.
A Method for Determining the Exceedance Envelope of Severe Spectrum Based on the Acceleration-exceedance Curves of Fokker 27 Airplanes
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(4): 840-845.
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[11] |
LIU Kege, YAN Chuliang.
Load Measurement and Compilation of Landing Gear of Airplane
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(5): 841-848.
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[12] |
He Xiaofan;Dong Yanmin;Liu Wenting.
Reliability Analysis on Fatigue Life with Separated Structural and Load Spectrum Scatters
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(4): 732-737.
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[13] |
Tian Zhaofeng;Yan Chuliang.
A Method to Design Aircraft Load Spectrum Resources Database Based on RIA Framework
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(10): 1889-1894.
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[14] |
Yu Miao;Yan Guang;Liu Kege.
Aircraft Load Spectrum Database Platform Media Management System Constructed with Ajax Technology
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2008, 30(6): 1586-1591.
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[15] |
Zhang Zhengping;Ren Fang;Feng Bingchu.
Noise Task of Aircraft—Resolve in Engineering
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2008, 29(5): 1207-1212.
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