DAMAGE MECHANICS FINITE ELEMENT METHOD FOR PREDICTION OF TOTAL FATIGUE LIVES OF METAL STRUCTURE MEMBERS

作     者：Zheng Xu-dong,Zhang Xing(Beijing University of Aeronautics and Astronautics,Beijing China) 

出 版 物：《Chinese Journal of Aeronautics》 (中国航空学报(英文版))

年 卷 期：1992年第4期

页      面：223-233页

核心收录：

主　　题：TOTAL DAMAGE MECHANICS FINITE ELEMENT METHOD FOR PREDICTION OF TOTAL FATIGUE LIVES OF METAL STRUCTURE MEMBERS NACA 

摘      要：Damage mechanics method is applied to studying fatigue problems of metallic *** governing equations of stress-damage field and finiteelement-additional loading method are ***,formulas of predictingfatigue crack formation and propagation lives of structural members are derived withdamage increment as step *** lives of typical notched plates with various geometricalparameters,made of 2024 and 7075 are *** results show that the agreementbetween theoretical S — N curves and experimental ones is very *** methodrequires short CPU time and can be applied to engineering practice.