STIFFNESS DESIGN METHOD OF SYMMETRICAL LAMINATES USING LAMINATION PARAMETERS

被引:86
作者
FUKUNAGA, H
SEKINE, H
机构
[1] Tohoku University, Department of Aeronautics and Space Engineering, Sendai
关键词
D O I
10.2514/3.11304
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
[No abstract available]
引用
收藏
页码:2791 / 2793
页数:3
相关论文
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AIAA JOURNAL, 1991, 29 (04) :641-646
[2]   LAYUP OPTIMIZATION AGAINST BUCKLING OF SHEAR PANELS [J].
GRENESTEDT, JL .
STRUCTURAL OPTIMIZATION, 1991, 3 (02) :115-120
[3]  
MIKI M, 1985, MAT SYSTEM, V4, P61
[4]  
Tsai SW, 1980, INTRO COMPOSITE MATE