日本航空宇宙学会誌
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
複合材料積層板の有限要素法解析のための境界条件処理法
小野原 薫
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ジャーナル フリー

1991 年 39 巻 447 号 p. 202-204

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This paper presents two boundary techniques which are useful for FEM analysis of composite laminates. One is a rotational symmetric boundary technique and the other is a quasi three-dimensional boundary technique. The use of the rotational symmetric boundary technique allows a smaller FEM model. With the use of the quasi three-dimensional boundary technique, quasi three-dimensional analysis of composite laminates can be performed on the conventional 3-D FEM program. These techniques can readily be adopted to FEM programs.

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© The Japan Society for Aeronautical and Space Sciences
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