Methodoffolding wing weightanalysis

Aviation technics and technology


Аuthors

Yarygina M. V., Popov Y. I.*

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

*e-mail: design101@mai.ru

Abstract

The paper describes some peculiarities of naval aircrafts and folding wing special. Theexperience of naval crafts design is presented; the classification of typical methods of folding wing design is made. There are described the factors influencing mass increase. The method of folding wing weight analysis is shown. The influence of each junction element on wing mass increase is detected.

Keywords:

wing; folding junction; mass; navalaircraft;axis.


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