Analytical stability estimation for a stiffened cylindrical shell with a hole under a complex loading

Аuthors

Safronov V. S.

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

e-mail: v.s.safronov@mail.ru

Abstract

A technique is presented as well as appropriate theoretical investigation results/or stability problem as applies to stiffened cylindrical shell with a hole under longitudinal compression and external pressure. Analytical expressions are derived to solve this stability problem.

Keywords:

stiffened shell, cut, stability, complex loading