Analysis of the influence payload mass to the aircrafts moment of inertia characteristics over axis OZ.

Аuthors

Dolgov O. S.^*, Kuprikov N. M.^**, Lyakishev M. A.^***

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

*e-mail: dolgov@mai.ru
**e-mail: nkuprikov@gmail.com
***e-mail: maximmai@mail.ru

Abstract

The paper describes new approaches of moment of inertia shape formation over axis OZ of future technology airplanes. Defined preferable zones of placing payload in a fuselage accordingly its mass. Rated regularities between the geometric characteristics of alternative variants of placing payload in the fuselage and the moment of inertia parameters over axis OZ of the whole aircraft.

Keywords:

moment of inertia; payload; layout, fuselage.

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