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
.
DOI: 10.7527/S1000-6893.2013.0201
[1] Venter G, Haftka R T, Chirehdast M. Response surface approximations for fatigue life prediction. AIAA-1997-1331,1997.
[2] Shim H J, Kim J K. Consideration of fatigue life optimization of pulley in power-steering system. Materials Science and Engineering: A, 2008,483-484: 452-455.
[3] Tang Y C, Zhou X H, Chen J. Preform tool shape optimization and redesign based on neural network response surface methodology. Finite Elements in Analysis and Design, 2008, 44(8): 462-471.
[4] Xue C J, Tan W, Xu F J, et al. Structural fatigue life optimization method based on response surface model. Journal of Nanjing University of Science and Technology, 2011, 35(6): 843-846. (in Chinese) 薛彩军, 谭伟, 徐奋进, 等. 基于响应面模型的结构疲劳寿命优化方法. 南京理工大学学报, 2011, 35(6): 843-846.
[5] Zhang C C, Yao W X. Anti-fatigue optimal design based on response surface model. Journal of Nanjing University of Aeronautics & Astronautics, 2007, 39(1): 37-40. (in Chinese) 张成成, 姚卫星. 基于响应面的结构抗疲劳优化设计方法. 南京航空航天大学学报, 2007, 39(1): 37-40.
[6] Liu G L, Shen H J, Ren L. Response surface model applicable to the fatigue optimal design of structures. Mechanical Engineering & Automation, 2009, 10(5): 61-63. (in Chinese) 刘根林, 沈海军, 任亮. 响应面模型在结构疲劳优化设计中的应用. 机械工程与自动化, 2009, 10(5): 61-63.
[7] Mrzyglod M, Zielinski A P. Parametric structural optimization with respect to the multiaxial high-cycle fatigue criterion. Structural and Multidisciplinary Optimization, 2007, 33(2): 161-171.
[8] Liu Y S, Liu J, Shao X J, et al. Effect of roughness on fatigue life of open holes. Key Engineering Materials, 2007, 348-349: 757-760.
[9] Goranson U G. Fatigue issues in aircraft maintenance and repairs. International Journal of Fatigue, 1997, 19(93): 3-21.
[10] Mohaghegh M. Evolution of structures design philosophy and criteria. Journal of Aircraft, 2005, 42(4): 814-831.
[11] Liu Y S, Yuan X K, Liu J, et al. Research on structure detail fatigue rating DFR and testing method. Experimental Technology and Management, 2008, 25(1): 27-29. (in Chinese) 刘永寿, 袁修开, 刘军, 等. 结构细节疲劳额定值DFR及其试验方法的研究. 实验技术与管理, 2008, 25(1): 27-29.
[12] Dong Y M, Liu W T, Yang C. Military aircraft durability design method based on detail fatigue rating. Acta Aeronautica et Astronautica Sinica, 2010, 31(12): 2357-2364. (in Chinese) 董彦民, 刘文珽, 杨超. 军用飞机结构耐久性设计的细节疲劳额定值方法. 航空学报, 2010, 31(12): 2357-2364.
[13] Huang X, Liu J Z, Ma S J, et al. Sensitivity analysis of the parameters in detail fatigue rating equation. Acta Aeronautica et Astronautica Sinica, 2012, 33(5): 863-870. (in Chinese) 黄啸, 刘建中, 马少俊,等. 细节疲劳额定强度计算参量取值敏感性研究. 航空学报, 2012, 33(5): 863-870.
[14] Yuan H S, Xu Z N. Analysis of internal force for joints by PATRAN/NASTRAN software. Civil Aircraft Design & Research, 2003(2): 15-18. (in Chinese) 袁华生, 徐仲年. 使用PATRAN/NASTRAN软件进行连接件内力分析. 民用飞机设计与研究, 2003(2): 15-18.
[15] Zhang C C, Yao W X, Ye B. Equivalent stress severity factor approach for fatigue of multi-fastener plate. Acta Aeronautica et Astronautica Sinica, 2009, 30(2): 271-275. (in Chinese) 张成成, 姚卫星, 叶彬. 连接件疲劳寿命分析的等效SSF法. 航空学报, 2009, 30(2): 271-275.