[1]TANAKA K. Engineering Formulae for Fatigue Strength Reduction Due to Crack-like Notches[J]. International Journal of Fracture,1983,22(2):39-46.
[2]TAYLOR D. Geometrical Effects in Fatigue: a Unifying Theoretical Model[J]. International Journal of Fatigue ,1999,21(5):413-420.
[3]辛朋朋,胡绪腾,宋迎东. 基于临界距离理论的TC4合金缺口试样低循环疲劳寿命预测[J].航空动力学报,2012,27(5):1105-1112.
XIN Pengpeng,HU Xuteng,SONG Yingdong. LCF Life Prediction for TC4 Alloy Notched Specimens Based on Theory of Critical Distance[J]. Journal of Aerospace Power,2012,27(5):1105-1112.
[4]LANNING D B,NICHOLAS T,HARITOS G K. On the Use of Critical Distance Theories for the Prediction of the High Cycle Fatigue Limit Stress in Notched Ti-6A1-4V[J]. International Journal of Fatigue,2005,27(1):45-57.
[5]NAIK R A,LANNING D B,NICHOLAS T. A Critical Plane Gradient Approach for the Prediction of Notched HCF Life[J]. International Journal of Fatigue,2005,27(5):481-492.
[6]姚卫星.金属材料疲劳行为的应力场强法描述[J]. 固体力学学报,1997,18(1):38-48.
YAO Weixing. Metal Material Fatigue Behavior Description of the Stress Field Intensity Method[J]. Acta Mechanica Solida Sinica,1997,18(1):38-48.
[7]尚德广,王大康,李明,等.随机疲劳寿命预测的局部应力应变场强法[J]. 机械工程学报,2002,38(1):67-70.
SHANG Deguang,WANG Dakang,LI Ming,et al. Random Fatigue Life Prediction of Local Stress-strain Field Intensity Method[J]. Chinese Journal of Mechanical Engineering,2002,38(1):67-70.
[8]郭平,陈波华,都昌兵.基于场强法的燃烧室机匣安装座疲劳寿命预测[J]. 航空发动机,2011,37(6):36-39.
GUO Ping,CHEN Bohua,DU Changbing. Based on the Approach of Field Intensity Combustion Chamber for Bushing after Installation of the Fatigue Life Prediction[J]. Journal of Aircraft Engine,2011,37(06):36-39.
[9]张成成,姚卫星. 典型缺口件疲劳寿命分析方法 [J]. 航空动力学报,2013,28(6):1223-1230.
ZHANG Chengcheng,YAO Weixing. Typical Fatigue Life Analysis Approaches for Notched Components[J]. Journal of Aerospace Power,2013,28(6):1223-1230.
[10]姚卫星. 结构疲劳寿命分析[M]. 北京:国防工业出版社,2003.
YAO Weixing. Fatigue Life Prediction of Structure[M]. Beijing: National Defence Industry Press,2003.
[11]COLLINS J A. Failure of materials in Mechanical Design:Analysis,Prediction,and Prevention[M]. 2nd ed. New York: Wiley Publication,1993.
[12]NEUBER H. Theory of Notch Stress, Principles for Exact Calculation of Strength with Reference to structural Form and Material[M].2nd ed. Berlin:Springer Verlag,1958.
[13]高镇同. 航空金属材料疲劳性能手册[M].北京:北京航空材料研究所,1981.
GAO Zhentong. Air Metal Material Fatigue Performance Handbook[M]. Beijing: Beijing Institute of Aeronautical Materials,1981.
[14]SIEBEL E,STIELER M. Significance of Dissimilar Stress Distributions for Cycling Loading[J]. VDI-Z,1955,97(5):121-126.
[15]项彬,史建平,郭灵彦,等. 铁路常用材料Goodman疲劳极限图的绘制与应用[J]. 中国铁道科学,2002,23(4):72-76.
XIANG Bin,SHI Jianping,GUO Lingyan,et al. Plotting and Application of Goodman Fatigue Limit Diagram of Railway Common Materials[J]. China Railway Science,2002,23(4):72-76.
[16]李舜酩.机械疲劳与可靠性设计[M]. 北京:科学出版社,2006.
LI Shunming. Mechanical Fatigue and Reliability Design[M]. Beijing: Science Press,2006.
[17]李海梅,宋刚,刘勇志.金属材料疲劳极限的估算[J].郑州大学学报:工学版,2002,23(4): 26-29,39.
LI Haimei,SONG Gang,LIU Yongzhi. Estimating Formula of Fatigue Limits for Metallic Materials[J]. Journal of Zhengzhou University: Engineering Science Edition,2002,23(4): 26-29,39.