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细观几何结构对复合材料初始屈服面的影响
引用本文:宋迎东,孙志刚,雷友锋,高德平.细观几何结构对复合材料初始屈服面的影响[J].航空动力学报,2004,19(6):749-754.
作者姓名:宋迎东  孙志刚  雷友锋  高德平
作者单位:南京航空航天大学,能源与动力学院,江苏,南京,210016;南京航空航天大学,能源与动力学院,江苏,南京,210016;南京航空航天大学,能源与动力学院,江苏,南京,210016;南京航空航天大学,能源与动力学院,江苏,南京,210016
基金项目:航空科学基金资助项目(01C52017)
摘    要:采用宏—细观统一的弹塑性本构模型分析了多轴载荷作用下不同纤维形状、不同纤维排列方式对金属基复合材料初始屈服面的影响。研究表明:在纵向正应力作用下,圆截面纤维复合材料的初始屈服应力基本上与方形截面纤维复合材料的初始屈服应力相等;不同纤维排列方式的复合材料初始屈服应力基本上相同。当存在横向应力或纵横剪切应力时,圆截面纤维复合材料初始屈服面在方形截面纤维复合材料初始屈服面之内;六角形排列时最容易屈服,而方形对角排列屈服应力最高。 

关 键 词:航空、航天推进系统  金属基复合材料  宏-细观本构模型  屈服面
文章编号:1000-8055(2004)06-0749-06
收稿时间:2003/11/4 0:00:00
修稿时间:2003年11月4日

Influence of Micro-Structural Geometry on Composite Initial Yielding Surfaces
SONG Ying-dong,SUN Zhi-gang,LEI You-feng and GAO De-ping.Influence of Micro-Structural Geometry on Composite Initial Yielding Surfaces[J].Journal of Aerospace Power,2004,19(6):749-754.
Authors:SONG Ying-dong  SUN Zhi-gang  LEI You-feng and GAO De-ping
Institution:College of Energy and Power Engineer,Nanjing University of Aeronautics and Astronautics,Nanjing210016,China
Abstract:The unified macro and micro mechanics constitutive model was used to investigate the influence of micro-structural geometry,such as fiber shape and fiber packing array,on the composite initial yielding surfaces under multi-axial loading.Under longitudinal stress,composites reinforced by fibers with square cross section have the same yielding stress as the ones reinforced by fibers with cyclic cross section.Fiber packing array has no effect on the yielding stress.In the presence of transverse or shear stresses, the composite initial yielding surface with square cross section fibers is inside of the one of composite with square cross section fibers.Composite with hexagon fiber array has the lowest yielding stress;however,composite with square-diagonal fiber array has the highest.
Keywords:aerospace propulsion system  metal matrix composite  marco and micro mechanics model  yielding surface
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