Analysis of technological residual stresses arising in multilayered composite panels that have asymmetric structure of composite's package along its thickness

The influence of technological pre-tension of fibers, orientation angles of composite layers and volume fraction of fibers and resin on the strength of the bearing layers of multilayered composite panels manufactured by the process of autoclaving are considered in this article. The results of a calculation of residual stresses in the layers of anisotropic plates with asymmetric structure along its thickness arising as result of the influence of technological factors are presented.