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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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| [2] |
WANG Binwen, CHEN Xiangming, DENG Fanchen, CHAI Yanan.
Complex load test technology for aircraft panels: Review
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(3): 24987-024987.
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| [3] |
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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ZHANG Min, TIAN Xitian, LI Bo.
Shape control for press bend forming of integral panels
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(7): 623620-623620.
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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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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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Liang Wei;Zhang Lichun;Wu Dafang;Wang Zhan;Mai Hanchao.
Computation and Analysis of Transient Thermal Performance ofMetal Honeycomb Sandwich Panels
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(4): 672-677.
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Jiao Guiqiong;Du Kai;Yang Chengpeng;Lu Zhixian.
Compressive Properties of Stiffened Composite Panels with Discretesource Damage
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2007, 28(6): 1383-1388.
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XU Ze;XU Xi-wu;ZENG Ning;LI Qiu-long.
The Research of Air Inlet Structure Integrity Assessment Technology
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2006, 27(3): 436-439.
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XUE Hong-qian;TAO Hua;C. BATHIAS.
The Design of Specimen for Fatigue Test at Ultrasonic Frequency
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2004, 25(4): 425-428.
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XUE Hong-qian;TAO Hua.
Investigation of Superhigh Cycle Fatigue Behavior on Nodular Cast Iron
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2004, 25(1): 93-96.
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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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Tao Hua .
PROGRESS OF ULTRASONIC FATIGUE
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1998, 19(2): 228-231.
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Ge sen;Cao Qi;Shao Chuang;Guo Dingwen.
NEW METHOD FOR OBTAINING SONIC FATIGUE S N CURVES AT ELEVATED TEMPERATURE
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(1): 75-77.
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Yao Jin.
A METHOD FOR DEVELOPING SONIC FATIGUE TEST SPECTRUM OF AIRCRAFT STRUCTURE
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(S1): 114-116.
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