| [1] |
Xiangtao MA, Fayao WANG, Yingjie ZHU, Peng HAO, Bo WANG, Guanri LIU.
Accelerated optimization design of stiffened cylindrical shell for imperfection tolerance
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(1): 226430-226430.
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| [2] |
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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| [3] |
GAO Wei, LIU Cun, CHEN Shunqiang.
Axial compression test and analysis method of composite stiffened plates with variable thickness
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526764-526764.
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| [4] |
XING Yufeng, LI Gen, YUAN Ye.
A review of closed-form analytical solution methods for eigenvalue problems of rectangular plates
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(10): 527333-527333.
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| [5] |
CAO Pengyu, NIU Kangmin.
Development of buckling model and failure criterion of sandwich structure
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 424669-424669.
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| [6] |
CHEN Xiangming, CHEN Puhui, SUN Xiasheng, WANG Binwen, WANG Zhe, ZHANG Hui, CHAI Yanan.
Buckling interaction formulae of composite plates under combined axial compression/tension and shear loads
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(12): 225417-225417.
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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] |
LI Zengcong, TIAN Kuo, ZHAO Haixin.
Efficient variable-fidelity models for hierarchical stiffened shells
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(7): 623435-623435.
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| [9] |
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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| [10] |
ZHANG Yongjie, WU Yingying, ZHU Shengli, WANG Bintuan, TAN Zhaoguang, YUAN Changsheng.
Buckling and progressive damage analysis of representative compressed PRSEUS panel in blended-wing-body civil aircraft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(9): 623185-623185.
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| [11] |
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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| [12] |
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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| [13] |
SHA Yundong, ZHANG Mohan, ZHAO Fengtong, ZHU Fulei.
Nonlinear response analysis and test verification for thin-walled structures to thermal-acoustic loads
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(4): 222544-222544.
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| [14] |
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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| [15] |
CHEN Yong, LIAO Gaojian, REN Lihai, LIU Xi.
Damage tolerance of GLARE laminates subjected to high-velocity impact
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(7): 221733-221733.
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