[1] 刘文光,陈国平,贺红林,等.结构振动疲劳研究综述[J].工程设计学报,2012,19(1):1-8. LIU Wen-guang,CHEN Guo-ping,HE Hong-lin,et al.Review of studying on vibration fatigue [J].Chinese Journal of Engineering Design,2012,19(1):1-8.
[2] 周江贝,孙秦.复合材料薄壁加筋结构局部稳定性分析的谱单元法[J].机械科学与技术,2014,33(2):1912-1915. ZHOU Jiang-bei,SUN Qin.The spectral element method of the local stability for the stiffened thin-walled structure of the composite [J].Mechanical Science and Technology for Aerospace Engineering,2014,33(2):1912-1915.
[3] 杨竣博,宋笔锋,钟小平.曲加筋条壁板优化设计研究[J].机械强度,2014,36(6):904-910. YANG Jun-bo,SONG Bi-feng,ZHONG Xiao-ping.Research on optimal design of curvilinearly stiffened panels [J].Journal of Mechanical Strength,2014,36(6):904-910.
[4] 郑洁,任善.复合材料加筋壁板稳定性分析方法研究[J].航空科学技术,2015,26(3):44-48. ZHENG Jie,REN Shan.Study on stability analysis method of composite stiffened plates [J].Aeronautical Science and Technology,2015,26(3):44-48.
[5] 王富生,张钧然,郑涵天,等.复合材料加筋壁板鸟撞动响应分析[J].振动与冲击,2013,32(4):6-10. WANG Fu-sheng,ZHANG Jun-ran,ZHENG Han-tian,et al.Dynamic response of a composite reinforced panel to bird strike [J].Journal of Vibration and Shock,2013,32(4):6-10.
[6] SAKANO M,WAHAB M A.Fatigue strength of welded transverse stiffener joints under variable amplitude loading[J].International Journal of Pressure Vessels and Piping,1998,75(15):1037-1045.
[7] 刘文光,贺红林.单向双筋板结构件共振疲劳试验及分析[J].实验力学,2012,27(3):361-367. LIU Wen-guang,HE Hong-lin.Resonance fatigue testing and analysis of one-way double-stiffened plate [J].Journal of Experimental Mechanics,2012, 27(3):361-367.
[8] 刘文光.考虑结构裂纹扩展的振动疲劳寿命计算方法[J].振动工程学报,2012,25(1):79-82. LIU Wen-guang.Calculation method of vibration fatigue life with structure crack growth [J].Journal of Vibration Engineering,2012,25(1):79-82.
[9] 顾超林.加筋板连接件的振动疲劳仿真研究[D].南京:南京航空航天大学航空宇航学院,2009:1-69. GU Chao-lin.Research on vibration fatigue of stiffened aluminum alloy panel [D].Nanjing:Nanjing University of Aeronautics and Astronautics,College of Aerospace Engineering,2009:1-69.
[10] 廉政.典型结构件的振动疲劳分析[D].南京:南京航空航天大学航空宇航学院,2010:1-55. LIAN Zheng.Vibration fatigue analysis of typical structure [D].Nanjing:Nanjing University of Aeronautics and Astronautics,College of Aerospace Engineering,2010:1-64.
[11] 王佳莹.考虑温度影响下结构振动疲劳寿命估算[D].南昌:南昌航空大学航空制造工程学院,2012:1-56. WANG Jia-ying.Estimation of structural vibration fatigue life with temperature involved [D].Nanchang:Nanchang Hangkong University,School of Aeronautic Manufacturing Engineering,2012:1-56.
[12] 濮良贵,纪名刚.机械设计[M].7版.北京:高等教育出版社,2001:1-210. PU Liang-gui,JI Ming-gang.Design of machinery[M]. 7th ed. Beijing:Higher Education Press,2001:1-210.
[13] 肖寿庭,杜修德.LY12CZ铝合金悬臂梁动态疲劳 S—N曲线的试验测定[J].机械强度,1995,17(3):21-24. XIAO Shou-ting,DU Xiu-de.Measurement of a dynamic fatigue S-N curve for LY12CZ Al alloy cantilever specimens [J].Journal of Mechanical Strength,1995,17(3):21-24. |