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Additional resources for The 1995-96 Yemen-Eritrea Conflict over the Islands of Hanish and Jabal Zuqar: a Geopolitical Analysis issue 66

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Some queries arise: 1. e. large scale, or overall) physical properties from those of the constituent materials? 2. Can the proportion of the constituent materials be varied to achieve a desired stiffness and strength for the composite? If it can, how can it be done best? 3. Can we analyze the internal fields in the heterogeneous medium? 4. Can we replace the piecewise constant heterogeneous medium by a homogeneous one by somehow smearing the heterogeneity? These questions show that there are two basic problems: determine the lamina properties by the procedures of micromechanics; use these properties in macromechanics for a global analysis of the continuum.

3: Axial and bending deformations of two cross-ply laminates laminates. ) • Angle-ply: If every layer has either angle () or angle -(), the laminate is said to be an angle-ply laminate. An example of an angle-ply 44 Composites laminate is (30/ - 30/30/ - 30), or simply (30/ - 30h. • Cross-ply: If every layer has either () = 0, or () = 90, the laminate is said to be a cross-ply laminate. A (0/90/0/90), or (0/90h, is an example of a cross-ply laminate. • Quasi-isotropic: If every layer has either () = 0, () = 90, () = +45, or () = -45, symmetrically arranged with respect to the middle surface, the laminate is said to be a quasi-isotropic laminate.

19) Matrix k N is the natural stiffness matrix. Once formed, simple congruent transformations transform it first to the local elemental and ultimately to the global cartesian coordinates. This general methodology, briefly described in this section, will be used extensively in the sequel for the derivation of the natural stiffness matrices for laminated composite beam, plate and shell elements. 3 31 Natural modes for selected finite elements The natural modes must satisfy all kinematic compatibility conditions at the boundaries.

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