ALTERNATE EXACT EQUATIONS FOR THE INEXTENSIONAL DEFORMATION OF ARBITRARY, QUADRILATERAL, AND TRIANGULAR PLATES

被引:12
作者
SIMMONDS, JG [1 ]
LIBAI, A [1 ]
机构
[1] TECHNION ISRAEL INST TECHNOL,DEPT AERONAUT ENGN,HAIFA,ISRAEL
来源
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME | 1979年 / 46卷 / 04期
关键词
D O I
10.1115/1.3424674
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Previously, a set of 9 exact differential equations was derived for the inextensional deformation of a plate bounded by two straight edges and two arbitrary curves. One straight edge is built-in. The other moves rigidly and is subject to a force and couple. The curved edges are stress-free. If the plate twists as it deforms, then, as shown herein, the 9 equations may be replaced by 7. The equations are written in a dimensionless form allowing a ready comparison with Mansfield’s theory that assumes small but finite angles of rotation. If the end load is a couple only, then an independent set of 5 equations emerges. These reduce to 4 for a quadrilateral plate. A numerical example compares the prediction of the exact equations against those of Mansfield. For triangular plates under tip forces only, an alternate, better conditioned, set of 9 differential equations is derived, and the behavior of the solutions near the tip is analyzed. © 1979 by ASME.
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页码:895 / 900
页数:6
相关论文
共 6 条
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[2]  
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[3]  
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[4]  
MANSFIELD EH, 1955, AIRCRAFT ENGINEERING, V21, P102
[5]  
SIMMONDS JG, UNPUBLISHED
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