The experimental calculated method of analysis for tail part of fuselage frame of integral composition fighter

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 experimental methods aimed for effective rational design of integral scheme fighter fuselage tail section parts are considered. Engine pod junction structure is subject to analysis with its forth section in case of spreadengines.

Keywords:

design, rib, beam, load, mass, operation factor