Designing of structural elements of the aircraft using the similarity criterion

Aviation technics and technology


Аuthors

Kicheev V. E.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

e-mail: m.oskb@yandex.ru

Abstract

The problem of designing of three different structural elements operating under static loading has been analyzed. The similarity criterions have been assigned. The limits of applicability of the design calculations formulas have been defined.

Keywords:

designing, bar, longeron, spar, panel, similarity criterion


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