Aircraft Engineering
Аuthors
1*, 2**, 21. ,
2. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
*e-mail: kaf309@mai.ru
**e-mail: emc@mai.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
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