Aircraft Engineering
Аuthors
,Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
Abstract
A conceptual design problem is considered as some optimization problem. An optimality criterion needed to solve this problem is interpreted as an estimation of a vehicle perfection grade. The optimality criterion is derived from results obtained by means analysis of application level for achievements of up-to-date technological progress. It is demonstrated that a quantitative assessment of a degree for the application level can be expressed through using efficiency of the vehicle mass.
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