航空学报 > 1990, Vol. 11 Issue (12): 597-601

复合材料结构分析系统YIDOYU-Ix

丁惠梁, 孙侠生, 王炜, 孙宪学   

  1. 飞机强度研究所
  • 收稿日期:1988-12-08 修回日期:1989-08-20 出版日期:1990-12-25 发布日期:1990-12-25

ANALYSIS SYSTEM OF COMPOSITE STRUCTURES(YIDOYU-I_X)

Ding Huiliang, Sun Xiasheng,Wang Wei, Sun Xianxue   

  1. Aircraft Strength Research Institute
  • Received:1988-12-08 Revised:1989-08-20 Online:1990-12-25 Published:1990-12-25

关键词: 结构分析, 优化设计, 结构剪裁, 复合材料叠层板

Abstract: To make full use of the inherent high specific strength and high specific stiffness of the composite materials, and to realize the possibility of "tailoring"composite structures for particular design reguirements, a large scale composite structural Analysis and Synthesis System (COMPASS) is being developed in order to improve aircraft per-formance and shorten its developing period. Based en a successful"Aircraft Multi-constraints Optimal Design System" (YIDOYU-1), its prototype reference system (called YIDOYU- I ,) has been developed first. In this paper, preliminary numerical experience gained is given, and analytical capability and the feasibility of"structural tailoring"are demonstrated.

Key words: structural analysis, optimal design, structural tailoring, composite laminate.