[1] WOODWARD J R.Titanium honeycomb sandwich fabrication process[C]//Fifth National SAMPLE Technical Conference,1973:432-437. [2] 谢宗蕻,岳喜山,孙俊锋.钛合金蜂窝壁板隔热性能试验研究[J].南京航空航天大学学报,2016,48(1):16-20.XIE Z H,YUE X S,SUN J F.Experimental study on thermal insulation performance of titanium honeycomb sandwich panels[J].Journal of Nanjing University of Aeronautics & Astronautics,2016,48(1):16-20(in Chinese). [3] 岳喜山,欧阳小龙,侯金保,等.钛合金蜂窝壁板结构钎焊工艺[J].航空制造技术,2009(10):96-98.YUE X S,OUYANG X L,HOU J B,et al.Brazing process of titanium alloy honeycomb sandwich panel structure[J].Aeronautical Manufacturing Technology,2009(10):96-98(in Chinese). [4] 静永娟,李晓红,岳喜山.TC1钛合金蜂窝夹层结构的钎焊工艺研究与分析[J].航空制造技术,2012(13):137-139.JING Y J,LI X H,YUE X S.Research and analysis of processing parameter for brazing honeycomb sandwich construction in titanium alloy[J].Aeronautical Manufacturing Technology,2012(13):137-139(in Chinese). [5] ZHAO W,XIE Z H,LI X,et al.Compression after impact behavior of titanium honeycomb sandwich structure[J].Journal of Sandwich Structures and Materials,2018,20(5):639-657. [6] XIE Z H,ZHAO W,HANG J T,et al.Low-velocity impact behavior of titanium honeycomb sandwich structures[J].Journal of Sandwich Structures and Materials,2018,20(8):1009-1027. [7] 刘晓宇.钛合金蜂窝夹层结构力学性能分析与试验验证[D].西安:西北工业大学,2014.LIU X Y.Mechanical properties of titanium honeycomb sandwich structures analysis and experimental validation[D].Xi'an:Northwestern Polytechnical University,2014(in Chinese). [8] ZENKERT D.An introduction to sandwich construction[M].London:Engineering Materials Advisory Services Ltd.,1995. [9] SHENOI R A,GROVES A, RAJAPAKSE Y D S.Theory and applications of sandwich structures[M].Southampton:University of Southampton Press,2005. [10] 王兴业.夹层结构复合材料设计原理及其应用[M].北京:化学工业出版社,2007.WANG X Y.Design principle and application of sandwich structure composite materials[M].Beijing:Chemical Industry Press,2007(in Chinese). [11] 杨凯,刘立武,于开平,等.带有典型缺陷的金属蜂窝夹层结构的剩余强度研究[J].固体火箭技术,2011,34(5):652-654.YANG K,LIU L W,YU K P,et al.Study on the residual strength of metal honeycomb sandwich structure with typical defects[J].Journal of Solid Rocket Technology,2011,34(5):652-654(in Chinese). [12] 赵震波,许希武,郭树祥.梯度钛合金裂纹扩展速率测试及梯度对扩展寿命影响[J].复合材料学报,2017,34(1):168-174.ZHAO Z B,XU X W,GUO S X.Fatigue crack growth rate determination of graded titanium alloys and the influence of gradient for propagation life[J].Acta Materiae Compositae Sinica,2017,34(1):168-174(in Chinese). [13] MAZEL V,DIARRA H,BUSIGNIES V,et al.Study of the validity of the three-point bending test for pharmaceutical round tablets using finite element method modeling[J].Journal of Pharmaceutical Sciences,2014,103(4):1305-1308. [14] 孔祥皓,赫晓东.带有典型缺陷的金属蜂窝夹层结构的共面力学性能研究[J].固体火箭技术,2010,33(6):684-689.KONG X H,HE X D.Study on coplanar mechanical properties of metal honeycomb sandwich structures with typical defects[J].Journal of Solid Rocket Technology,2010,33(6):684-689(in Chinese). [15] HUANG X,RICHARDS N L.Activated diffusion brazing technology for manufacture of titanium honeycomb structures-A statistical study[J].Welding Research,2004,83(3):73-81. [16] ALLEN H G.Analysis and design of structural sandwich panels[M].Oxford:Pergamon Press,1969. [17] 杨宇.金属蜂窝夹层结构弯曲性能分析[J].科技视界,2015(26):104-105.YANG Y.Bending property analysis of metal honeycomb sandwich structure[J].Science & Technology Vision,2015(26):104-105(in Chinese). [18] 上海玻璃钢研究所,北京航空材料研究院.夹层结构弯曲性能试验方法:GB/T 1456-2005[S].北京:中国标准出版社,2005.Shanghai FRP Research Institute,Bejing Institute of Aeronautical Materials.Test method for flexural properties of sandwich constructions:GB/T 1456-2005[S].Beijing:China Standard Press,2005(in Chinese). [19] 郭玉瑛.飞机设计手册第三册:材料(上)[M].北京:航空工业出版社,1997:405.GUO Y Y.Aircraft design manual three:Material(1)[M].Beijing:Aeronautical Industry Press,1997:405(in Chinese). |