Maneuverable aircraft face design under the cost limitation conditions

Аuthors

Kuprikov M. Y.^*, Komissarov A. A.

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*e-mail: kuprikov@mai.ru

Abstract

This article is dedicated to the peculiarities of the maneuverable aircraft face design process under the cost limitation conditions. An object of analysis is a vector of technical characteristics that can be modified by the airframe cost limits. It examines mathematical models that determine the cost of the aggregate taking into account its’ technical characteristics.

Keywords:

design; mass; cost; airframe; parameters.

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