RIGOROUS SOLUTION FOR AXIALLY-COMPRESSED CYLINDRICAL PANELS
Eliseu Lucena Neto1; Francisco Alex Monteiro1; Paulo de Tarso Soares1
1 Instituto Tecnológico de Aeronaútica
Baixar PDF doi:10.20906/CPS/CILAMCE2015-0032
Resumo
An exact solution, based on Lévy method, is presented for the linear buckling of axially compressed circular cylindrical panels with stringers attached to the straight edges. The boundary conditions differ from the classical simply supported ones by taking into account the torsional and warping rigidities of the stringers. The reported exact buckling solutions may be valuable as benchmark data.
Palavras-chave: Exact solution; Cylindrical panels; Buckling analysis