Methods of influence technological errors on stress-strain state of multilayered composite panels

Method for stress-strain state of composite materials and structures subject to technological influences is considered. We analyzed the influence of the magnitude of the difference between curing temperature and operating temperature, the angles of off-orientation in the monolayer and thickness of the composite panel in the distribution of the intensity of normal and shear stresses, as well as in the distribution of the maximum deflection in the multilayered composite panel.