[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] |
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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[4] |
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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[5] |
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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[6] |
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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[7] |
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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[8] |
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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[9] |
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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[10] |
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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[11] |
LIU Shuangyan, LI Yulong, XUE Pu, SHI Xiaopeng.
Effect of crack parameters and stiffener layout on dynamic stress intensity factor of 3×3 grid stiffened panel at resonance
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(1): 221423-221423.
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[12] |
NI Yang, XU Yuanming.
Stability of metallic sub-stiffened structure and its optimization under uniaxial loading
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(5): 1511-1519.
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[13] |
GU Xingjin, XU Xiwu.
Numerical Simulation of Damage in Stiffened Integral Composite Panels Under High Velocity Impact
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(2): 258-272.
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[14] |
LI Ya-zhi;ZHANG Xiang.
An Analysis of Fail-Safety and Fracture Control of Integrally Stiffened Panels
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(5): 842-846.
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[15] |
ZHENG Jin-xin;CUI Wei-cheng.
CALCULATING METHOD FOR THE EFFECTIVE WIDTH OF IMPERFECT STIFFENED PANEL PLATING WITH TRANSVERSE LOAD
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2002, 23(1): 48-50.
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