Design and Preparation of Curved Stainless Steel/Glass-Ceramics Laminated Composite Material

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Design and Preparation of Curved Stainless Steel/Glass-Ceramics Laminated Composite Material
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Key words:共形天线%不锈钢/微晶玻璃复合材料%微晶玻璃

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[2]Zhu Dan,Wang Yaoxian,Zhang Xinglu,Cheng Shujun.Properties of UHMWPE/PCH Composite Material[J].Aerospace Materials & Technology,2009,39(1).

[3]Preparation and Properties of High Temperature Oxidation Resistant BSAS Coatings on C/SiC Composite Material[J].Aerospace Materials & Technology

[4]Feng Zhenyu,Zou Tianchun,Hao Peng,Du Hongzeng,Tian Xiuyun.Determination Methods for Material and Design Allowables of Composite Aircraft Structure[J].Aerospace Materials & Technology,2011,41(5).

[5]HOU Gen-liang,SU Xun-jia,WANG Yan-bin,ZHOU Xiao-bo.Preparation of Anti-ablation HfC Coating on C/C Composite Material[J].Journal of Aeronautical Materials,2009,29(1):77-80.

[6]Wu Chengsi,Li Qingfei.Structure Design of Large Camber Composite Material Based on CATIA[J].Hongdu Science and Technology,2008(2):1-5.

[7]Xiong Pan,Qin Lijun,Liu Aibing,Wu Zaofeng,Zhang Liwei.Weight Reduction Design of Composite Material Tail Fairing[J].Hongdu Science and Technology,2015(1):65-68.

[8]Qin Li.The Optimum Parameter Design of Composite Material Joimts[J].Journal of Shenyang Institute of Aeronautical Engineering,1998,15(1):29-35.

[9]Yang Wentao,Wang Zhuanli.Application of Msc/Nastran in Buckling Analysis of Laminated Composite Sheet[J].Hongdu Science and Technology,2007(3):12-16.

[10]ZHANG Ji-kui,LI Zheng-neng,KOU Chang-he.Structural Design of High Aspect Ratio Composite Material Wing[J].Acta Aeronautica et Astronautica Sinica,2005,26(4):450-453.

[11]LI Yu-feng,JIN Qing-chen and LIU Zhi-dong.Filament-Wound Design and ANSYS Analysis for Composite Material High-Pressure Vessel[J].Journal of Propulsion Technology,2013,34(7):968-976.

[12]Lin Sen,He Xiang,Cong Hao.Buckling FEM and Strengthen Design on Hole of Composite Material Web[J].Civil Aircraft Design and Research,2013(Z2).

[13]林森、何翔、丛昊.Buckling FEM and Strengthen Design on Hole of Composite Material Web[J].Civil Aircraft Design and Research,2013(5):32.

[14]ZAHNG Hong,SUO Tao,LI Yu-long.Mechanical Behavior of a Stainless Steel Material at Elevated Temperatures and High Strain Rates[J].Journal of Aeronautical Materials,2012,32(1):78-83.

[15]Cheng Jialin.Design of Composite Laminated Joint and Its Application in Large Aircrafts[J].Acta Aeronautica et Astronautica Sinica,2008,29(3):640-644.

[16]Wang Qiang,Wang Jianhua,Li Xiaobao,Guo Dandan.Analysis and Improvement on Laminated Cracking of Circular Composite Joint[J].Hongdu Science and Technology,2013(2):62-65.

[17]LI Lin.Comparison Between Metal/Composite Material of Center Wing Box Design for Commercial Aircraft[J].Civil Aircraft Design and Research,2017(1):45.

[18]QING Guang-hui,ZHANG Ling,JIA Li-bin.Response Analysis of Composite Laminated Thermoelastic Plate[J].Journal of Civil Aviation University of China,2008,26(3):20-25.

[19]Wu Ping,Wan Jianping,Gan Wankui.The Study on the Repairing Process of Resin Base Composite Material Laminated Board z[J].Hongdu Science and Technology,2011(3).

[20]Lu Binghe,Li Ping and Zhang Junwei.Research Stiffened Structure Configuration of Laminated Composite Fuselage Based on Patran / Nastran and Hypersizer[J].Civil Aircraft Design and Research,2012(2):53-56.

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