宇航材料工艺
宇航材料工藝
우항재료공예
AEROSPACE MATERIALS & TECHNOLOGY
2010年
1期
19-23
,共5页
李海斌%阳建红%石增强%钟建强
李海斌%暘建紅%石增彊%鐘建彊
리해빈%양건홍%석증강%종건강
移动窗口%复合材料%局部应力
移動窗口%複閤材料%跼部應力
이동창구%복합재료%국부응력
Moving-window%Composite materials%Local stress
基于数字图像技术,获得非均匀复合材料的真实截面图像,以移动窗口方法依次选取截面中局部区域作为细观力学计算的单个胞元,结合改进的FVDAM方法获得复合材料的局部性能场,最后将得到的材料性能场输入有限元分析模型,求得复合材料在宏观载荷作用下的局部响应,为分析复合材料结构由于局部行为导致的失效提供了新的思路.
基于數字圖像技術,穫得非均勻複閤材料的真實截麵圖像,以移動窗口方法依次選取截麵中跼部區域作為細觀力學計算的單箇胞元,結閤改進的FVDAM方法穫得複閤材料的跼部性能場,最後將得到的材料性能場輸入有限元分析模型,求得複閤材料在宏觀載荷作用下的跼部響應,為分析複閤材料結構由于跼部行為導緻的失效提供瞭新的思路.
기우수자도상기술,획득비균균복합재료적진실절면도상,이이동창구방법의차선취절면중국부구역작위세관역학계산적단개포원,결합개진적FVDAM방법획득복합재료적국부성능장,최후장득도적재료성능장수입유한원분석모형,구득복합재료재굉관재하작용하적국부향응,위분석복합재료결구유우국부행위도치적실효제공료신적사로.
Based on digital image technique, true sectional image of heterogeneous composite materials was ob-tained. By selecting local region of the section as individual cell for micromechanics characterization, local property field of material was acquired with the use of moving-window technique in sequence combined with improved FVDAM (finite volume direct averaging method) ,then local property field is used in FEM ,loal stress is estimated in condition of macro-load,which presents a new way of thinking in analyzing failure of composite due to local behavior.