| [1] |
Liang MENG, Jinyuan YANG, Zhiwei YANG, Tong GAO, Hongquan LIU, Weihong ZHANG.
Buckling⁃resisting optimization design of typical aircraft panel and test validation
[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(5): 529679-529679.
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| [2] |
Junchao YANG, Xueming WANG, Xiangming CHEN, Peng ZOU, Zhe WANG.
Effect of low-velocity impact damage on compressive properties of composite stiffened panels
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(20): 228498-228498.
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| [3] |
Yunhe ZHAO, Shengnan WANG.
Solution to stress intensity factor by weight function method based on deep learning
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(19): 228367-228367.
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| [4] |
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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| [5] |
FENG Zhenyu, CHAI Chongbo, ZOU Jun, MOU Haolei.
Three-dimensional finite element analysis of stress intensity factors of butt-joints with multiple site damage
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524250-524250.
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| [6] |
DUAN Jiatong, SUI Fucheng, LIU Hanhai, XIE Fang, OUYANG Tian, BAO Rui.
Fatigue crack growth performance of thin-walled structure under bending load
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524326-524326.
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| [7] |
WANG Binwen, AI Sen, ZHANG Guofan, NIE Xiaohua, WU Cunli.
Validation method for post-buckling analysis model of stiffened composite panels considering uncertainties
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(8): 223987-223987.
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| [8] |
PENG Yilin, MA Yu'e, ZHAO Yang, ZHU Liang.
Shear buckling performance of Al-Li alloy stiffened panels
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(11): 423729-423729.
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| [9] |
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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| [10] |
LIU Cun, ZHANG Lei, YANG Weiping.
Post-buckling study and test verification of carrier-based aircraft wing stiffened panels under shear load
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(4): 622300-622300.
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| [11] |
ZHANG Yanjun, ZHU Liang, YANG Weiping, LI Xiaopeng, LEI Xiaoxin.
Buckling fatigue test of fuselage stiffened panel for carrier-based aircraft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(4): 622276-622276.
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| [12] |
XIONG Wenlei, SU Jiazhi, LIU Xiaolin, HAN Xiaoyong, QI Jingge, SONG Tiancheng.
Stringer deformation problems of panels stiffened with hat stringer in autoclave process
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(12): 423108-423108.
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| [13] |
TIAN Shuo, SHANG Jianqin, GAI Pengtao, CHEN Fulong, ZENG Yuansong.
Numerical simulation and deformation prediction of stress peen forming for integrally-stiffened panels
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(10): 422847-422847.
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| [14] |
ZHAO Xiaochen, WU Xueren, TONG Dihua, XU Wu, CHEN Bo, HU Benrun.
Accurate analytical weight function solutions for crack at edge of circular hole in infinite plate
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(9): 221976-221987.
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| [15] |
LI Zhenghong, XU Wu, ZHANG Xiaojing, YU Yin.
Experimental and analytical analyses of fatigue crack growth in sheets with multiple holes and cracks
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(7): 221867-221867.
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