Abstract
The process of designing airframe assemblies solves the problem of creating an optimal design in terms of quality that ensures the fulfillment of a wide range of highly conflicting requirements. Key requirements include: • provision of high quality of complex shape of the outer (aerodynamic) surface of the units, especially the wing and plumage. • providing strength from the effects of external and internal loads. • provision of a given resource and design life • ensuring the manufacturability of the production and operation of the structure, its maintainability, etc. At the same time, the satisfaction of basic requirements should be ensured with a minimum weight (weight) of the unit design.
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