[1] |
WAN Aoshuang.
Probabilistic assessment on damage tolerance of composite helicopter horizontal tail structure
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 525557-525557.
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[2] |
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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[3] |
WANG Tianshuai, HE Xiaofan, WANG Jinyu, LI Yuhai.
Estimation method for DFR value of DED-TA15 titanium alloy based on bimodal lognormal distribution
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(3): 225013-225013.
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[4] |
LIU Zongxing, LIU Jun, LI Weina.
Dynamic response and failure of typical fuselage structure under blast impact load
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(2): 224252-224252.
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[5] |
YOU Lingfei, ZHANG Jianguo, ZHOU Shuang, DU Xiaosong.
A new method for fatigue reliability calculation of aero-engine limited life parts
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(12): 223228-223228.
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[6] |
DONG Anqi, ZHAO Xinqing, ZHAO Yan.
Tension-tension fatigue performance of unidirectional out-of-autoclave composite manufactured by automated fiber placement
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(2): 421422-421422.
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[7] |
CHEN An, WEI Yulong, LIAO Jianghai, DONG Dengke, WANG Xu.
Damage tolerance test of stiffened fuselage panel under complex load
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(1): 420093-420093.
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[8] |
HAO Yanguang, LIU Jianzhong, GUO Xiang, LIU Hu, SHANG Deguang.
Residual strength prediction of welded stiffened thin-walled structures made of Al 6156-T4 alloy based on CTOD method
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(3): 827-833.
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[9] |
CHEN Binqi, ZENG Jianjiang, WANG Yiding, TONG Mingbo.
Application of DFR Method to Optimal Fatigue Design of Structures
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(5): 1122-1128.
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[10] |
Lin Zhiyu;Xu Xiwu.
Residual Compressive Strength of Stiffened Composite Laminates with Impact Damage
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(1): 56-61.
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[11] |
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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[12] |
REN Ke-liang;LU Guo-zhi;ZHANG You-hong.
Stochastic Arrange and Computer Simulation of Corrosion Pitting in Damage Structure
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(3): 459-462.
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[13] |
ZHANG You-hong;LU Guo-zhi;CHEN Yue-liang;.
Predicting Fatigue Life From Pre-corroded LY12-CZ Aluminium Test
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2005, 26(6): 779-782.
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[14] |
ZHANG Zhi-lin;YAO Wei-xing;FU Xiang-jiong.
Investigation on Scratch Tolerance of the Cabin Glass
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2004, 25(6): 569-572.
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[15] |
ZHAO Mei-ying;SUN Xiao-bo;Wan Xiao-peng.
Strength Investigation of Repaired Composite Honeycomb Structure with Unbonded Damage
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2003, 24(5): 474-476.
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