Abstract
The article describes a method for the synthesis of a finite element model of a wing with a strut for regional aircraft of the transport category. The method is based on the functional principle of decomposition, in which the general wing model is synthesized from individual models of substructures, which include the detachable part of the box and the wing strut. It is shown that, thanks to the use of the method of automated synthesis, it significantly reduces the amount of data entered "manually", which makes it possible to reduce the synthesis time and reduce the probability of errors.
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