The influence of arrangement of joist and ring parts of power frame 'to distribution of mass and load

Аuthors

Popov Y. I.^*, Stoljarov D. V.^**

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

*e-mail: design101@mai.ru
**e-mail: amidvoryalots@mail.ru

Abstract

Herein strength and parametric analysis methods aimed for quality definition for fuselage tail section lateral axis based structures are considered relative to integral scheme fighter. Full-scale power rib is subject to analysis with ring located around engine pod section of twin engine airplane with spread engines.

Keywords:

design, rib, load, the eccentricity, extension, mass, operation factor