While previous papers dealt with the accuracy of these interface stresses, in the present paper the accuracy and validity of displacements and stresses are established on classical benchmark bending examples for composites and sandwich plates.
Numerical examples are conducted for composite and porous materials with a variety of microscopic architectures to demonstrate the potential of the model.
For example, for a composite cost of I$10 per vaccinated girl, we assumed three doses of vaccine at $2.00 each; wastage of $0.90; freight and supplies of $0.59; administration of I$0.50; and immunisation support and programmatic costs of I$2.00.
Numerical examples for homogeneous and composite structures are presented to illustrate the proposed formulation.
A capability of the method was presented by numerical examples for two-phase composite made of alumina and zirconia (with different volume contents) and porous alumina subjected to a simple tension process.
Moreover, the morphology of the cells in groups A and B also appeared to be different compared to that of groups C and D. For example, after composite cultivation for 4 h, cell adhesion was observed for groups C and D, and the cells appeared to be oval or round in morphology, while less cells adhesion was apparent in groups A and B at this time.
Results will be used to determine the applicability of these materials for reuse in, for example, composite construction materials.
Also, this interaction could be more complex when the HRE also contains binding sites for nonreceptor factors, for example, composite HREs.
The efficiency of the proposed method is investigated through two numerical examples for isotropic and laminated composite plates.
For example, the Young's modulus for composite nanofibers with 1 % of CNTs content was 145.53 MPa as compared to 76.50 MPa for PLGA/1 % CNTs and 142.25 MPa for PLGA/2 % CNTs nanofibers.
