航空学报 > 1986, Vol. 7 Issue (6): 575-585

全各向异性圆柱形叠层长曲板在联合载荷下的稳定性

樊世荣   

  1. 飞机结构强度研究所
  • 收稿日期:1986-01-25 修回日期:1900-01-01 出版日期:1986-12-25 发布日期:1986-12-25

STABILITY OF LAYERED ANISOTROPIC LONG CYLINDRICAL PANELS UNDER COMBINED LOADING

Fan Shirong   

  1. Institute of Aircraft Structural Mechanics
  • Received:1986-01-25 Revised:1900-01-01 Online:1986-12-25 Published:1986-12-25

摘要: 本文给出了全各向异性圆柱形叠层长曲板在轴压、侧压和剪切载荷联合作用下稳定性的准确解。每个直边的边界条件可以是任意的。两直边边界条件可以不同。作为算例,研究了边界条件对各向同性圆柱长曲板剪切稳定性的影响。

Abstract: A theoretical analysis of buckling of layered anisotropic long cylindrical panels under combined axial, radial and shear loads is presented. The boundary conditions can be different at each straight edge.As an example, the influence of boundary conditions on stability of long cylindrical curved panel subjected to shear has been studied.