1997
DOI: 10.1016/s0263-8223(97)00073-1
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Nonlinear closed-form high-order analysis of curved sandwich panels

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Cited by 46 publications
(38 citation statements)
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“…A typical construction of a beam consists of two skins and a core. Numerous references can be found in literature covering the debonding problem (Frostig, 1992), buckling problem (Librescu and Hause, 2000), and dynamic mechanical problem of curved (Bozhevolnaya and Frostig, 1997) or non-curved beams (Frostig and Baruch, 1994). Many works proved that the transverse flexibility of the core affects the overall behaviors of sandwich beams, such as stresses and displacements (Librescu and Hause, 2000;Frostig and Baruch, 1994).…”
Section: Introductionmentioning
confidence: 99%
“…A typical construction of a beam consists of two skins and a core. Numerous references can be found in literature covering the debonding problem (Frostig, 1992), buckling problem (Librescu and Hause, 2000), and dynamic mechanical problem of curved (Bozhevolnaya and Frostig, 1997) or non-curved beams (Frostig and Baruch, 1994). Many works proved that the transverse flexibility of the core affects the overall behaviors of sandwich beams, such as stresses and displacements (Librescu and Hause, 2000;Frostig and Baruch, 1994).…”
Section: Introductionmentioning
confidence: 99%
“…In recent years, the effects of incorporating a vertical flexible core on the local and overall behavior of the flat and curved sandwich panels have been implemented through the use of the high-order theory (HSAPT); see [Frostig et al 1992] for flat panels, [Bozhevolnaya and Frostig 1997] for nonlinear behavior, [Bozhevolnaya 1998] on shallow sandwich panels, [Karayadi 1998] on cylindrical shells, [Frostig 1999] on the linear behavior of curved sandwich panels, [Bozhevolnaya and Frostig 2001] on the free vibration of curved panels, and [Thomsen and Vinson 2001] on composite sandwich aircraft fuselage structures.…”
Section: Antecedentsmentioning
confidence: 99%
“…The field equations and the boundary conditions are derived following the steps of the HSAPT approach for the curved sandwich panel [Frostig 1999;Bozhevolnaya and Frostig 1997]. The field equations are derived using the variational principle of extremum of the total potential energy:…”
Section: Mathematical Formulationmentioning
confidence: 99%
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“…Their theory does not impose any restriction on the deformation distribution through the thickness of the core. Bozhevolnaya and Frostig (1997) studied the static analysis of open single curved sandwich panels and uses high order theory to demonstrate the influence of the geometrical nonlinearity on the overall and local behaviors of the sandwich panel. The postbuckling analysis of geometrically imperfect anisotropic sandwich doubly-curved panels under compressive edge loads and a lateral pressure was done by Hause et al (1998) who assumed the core and the face sheets to be incompressible in the transverse normal direction.…”
Section: Introductionmentioning
confidence: 99%