Modelling of deformation of the flat aviation designs, reinforced by two curvilinear fibres families

Properties of the general resolving equations of a elasticity flat problem for a material reinforced with two families of fibres are analysed. Families of fibres are located in directions of curvilinear trajectories. The offered technique allows to investigate boundary problems for families equally intense and not extensible fibres with various elastic properties. Dependences of solutions on a choice of boundary density of reinforcing, and the form of a contour are received.