The applications of skew plates in the construction of aerospace structures are well known. The critical buckling load and post-buckling strength are two important design parameters of skew composite laminates. In this study, the refined buckling and nonlinear postbuckling solutions of a homogenous isotropic skew plate based on polynomial expansions of various degrees have been examined. Numerical results based on high-order Rayleigh-Ritz solutions are presented for certain type of oblique plates.
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Tianjin Univ, Sch Mech Engn, Tianjin 300072, Peoples R ChinaTianjin Univ, Sch Mech Engn, Tianjin 300072, Peoples R China
Tian, Y.
Wei, R.
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Tianjin Univ, Sch Mech Engn, Tianjin 300072, Peoples R ChinaTianjin Univ, Sch Mech Engn, Tianjin 300072, Peoples R China
Wei, R.
Eichhorn, V.
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Carl von Ossietzky Univ Oldenburg, Div Microrobot & Control Engn, D-26111 Oldenburg, GermanyTianjin Univ, Sch Mech Engn, Tianjin 300072, Peoples R China
Eichhorn, V.
Fatikow, S.
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Carl von Ossietzky Univ Oldenburg, Div Microrobot & Control Engn, D-26111 Oldenburg, GermanyTianjin Univ, Sch Mech Engn, Tianjin 300072, Peoples R China
Fatikow, S.
Shirinzadeh, B.
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Monash Univ, Dept Mech & Aerosp Engn, Robot & Mechatron Res Lab, Clayton, Vic 3800, AustraliaTianjin Univ, Sch Mech Engn, Tianjin 300072, Peoples R China
Shirinzadeh, B.
Zhang, D.
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Tianjin Univ, Sch Mech Engn, Tianjin 300072, Peoples R ChinaTianjin Univ, Sch Mech Engn, Tianjin 300072, Peoples R China