作者: D.J. Dawe , T.J. Craig
DOI: 10.1016/0020-7403(88)90063-X
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摘要: Abstract A finite strip method is presented for the determination of buckling stresses and natural frequencies vibration prismatic plate structures assembled from flats, which generally are laminates fibre-reinforced composite material. The single-term type, corresponding to assumption sinusoidal longitudinal spatial variation displacement force quantities. Anisotropic material behaviour applied in-plane shear stress accommodated by expressing field in terms complex out-of-plane properties flats based upon use first-order deformation theory. family models described a sub-structuring procedure utilised reduce size eigenvalue problem. Presented numerical results reveal high accuracy good convergence characteristics method, as well indicating influence through-thickness effects range circumstances.