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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1986, Vol. 7 ›› Issue (6): 575-585.

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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

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.