DTIC AD0728834: The Effects of Interlaminar Shear pdf

DTIC AD0728834: The Effects of Interlaminar Shear

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A small deflection plate theory is developed which includes higher order approximations to the effects of transverse shear. The governing equations and associated boundary conditions are developed by a variational method. The theory is sufficiently general to encompass anisotropic, laminated, composite, circularly curved, cylindrical plate elements of nonsymmetric cross section. Specific applications are made to the bending and the axial compression buckling of simply supported flat plates and to the axial compression buckling of curved plates and shells having classical, simple supports. It is shown that the effects of interlaminar shear can be significant in composite constructions which use very high strength fiber reinforcement

• Creator/s: Defense Technical Information Center
• Date: 5/1/1971
• Year: 1971
• Book Topics/Themes: DTIC Archive, Durlofsky, Harold, STANFORD UNIV CA DEPT OF AERONAUTICS AND ASTRONAUTICS, *BENDING, *COMPOSITE STRUCTURES, BUCKLING, DEFORMATION, FIBERS, LAMINATES, SHEAR PROPERTIES, SHELLS(STRUCTURAL FORMS

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