BUCKLING OF CYLINDRICAL PANELS BY A RITZ SCHEME
Lucas Nobumichi Yshii1; Rafael Christovão Santana1; Francisco Alex Correia Monteiro1; Eliseu Lucena Neto1
1 Instituto Tecnológico de Aeronaútica
doi:10.20906/CPS/CILAMCE2017-0613
Resumo
A Ritz scheme is proposed for the linear buckling of circular cylindrical panels with stringers attached to the straight edges. Boundary conditions differ from the classical simply supported ones in the sense that the torsion resisted by the stringers is also taken into account. The Ritz bases are generated from an appropriate integration of the Legendre polynomials. Benchmark data verify the effectiveness of the formulation.
Palavras-chave: Ritz method; Cylindrical panels; Buckling analysis