曲线坐标
极限抗拉强度
纤维
复合数
点(几何)
结构工程
材料科学
屈曲
复合材料
数学
工程类
几何学
作者
M. W. Hyer,R. F. Charette
出处
期刊:AIAA Journal
[American Institute of Aeronautics and Astronautics]
日期:1991-06-01
卷期号:29 (6): 1011-1015
被引量:291
摘要
'I'his paper investigates the gains in structural efficiency that can be achieved by aligning the fibers in some or all of the layers in a laminate with the principal stress directions in those layers. The name curvilinear fiber format is given to this idea. The problem studied is a plate with a central circular hole subjected to a uniaxial tensile load. An iteration scheme is used to find the fiber directions at each point in the laminate. Two failure criteria are used to evaluate the tensile load capacity of the plates with a curvilinear format, and for comparison, counterpart plates with a conventional straightline fiber format. The curvilinear designs for improved tensile capacity are then checked for buckling resistance. It is concluded that gains in efficiency can be realized with the curvilinear format.
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