航空学报 > 1996, Vol. 17 Issue (S1): 109-113

自适应复合材料薄壁梁形状控制

晏飞   

  1. 航空工业总公司603研究所, 西安, 710089
  • 收稿日期:1995-04-23 修回日期:1995-11-16 出版日期:1996-11-25 发布日期:1996-11-25

ADAPTIVE COMPOSITE CLOSED CELL THIN WALLED BEAM SHAPE CONTROL

Yan Fei   

  1. Strength Department,603 Design and Research Institute,Xian,710089
  • Received:1995-04-23 Revised:1995-11-16 Online:1996-11-25 Published:1996-11-25

摘要: 针对翼面和桨叶等升力面结构,以单闭室薄壁梁为典型结构模型,讨论自适应复合材料薄壁梁的弯曲和扭转,探讨控制结构形状的途径

关键词: 自适应复合材料, 结构形状控制, 薄壁梁

Abstract: An analytical model of arbitrary cross section uniform single closed cell anisotropic beams is developed.The bending and torsion as well as displaced shape control of the adaptive composite single closed cell thin walled beam are examined.

Key words: adaptive composite structure, shape control, thin-walled beam

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