Increasing the strength of the wing structureaircraft based on the use of metal-polymer composite material

Abstract

In the modern aviation industry, the task of increasing the structural strength of the aircraft wing is being actualize. The author presents an engineering methodology for power calculation and design of composite aircraft structures based on the analysis of strength characteristics of metal and metal-polymer composite materials. The paper uses theoretical and empirical research methods, as well as the results of foreign and domestic scientific materials.