General calculation model of split bar for lateral bending analysis of the wing panel stringers

Аuthors

Gromov V. F.^1*, Makarov A. F.², Korzun A. V.³

1. ,
2. Dubna International University for Nature, Society and Man, 141980 Moscow region, Dubna, Universitetskaya str., 19
3. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: vikirin@mail.ru

Abstract

The article contains the calculation model analysis of panel deformation estimation (in its surface) from stringer joint riveting. Possibility to use a theory of split bar on the elastic foundation.

Keywords:

: panel, skin, stringer, deformation, fastening.