Static analysis of honeycomb sandwich structure

Sandwich structure possess one or more than one layers which are stiff in nature with a core having flexibility. Facings have the capability to carry load, which comes from the core. There are several sandwich structure available with variety of applications. Due to weight sensitive these structures are used in aircraft and satellites. Honeycomb sandwich structure with angle 30 have been modelled and analysis had done and results are obtained and graphs have been plotted between displacement-w and length of facesheet of honeycomb structure, analysis have done on honeycomb sandwich structure with different support conditions like cccc (all edges clamped), scsc (opposite edges are in same support condition), hhhh
(all edges are in hinged conditions), ssss (all edges are in simply supported conditions) and it has been observed that cccc condition gives less displacement compared with ‘scsc’, ‘hhhh’, ‘ssss’. Analysis had carried out on honeycomb structure under different loadings such as point load, UDL, Pressure load and it
has been observed that the deformation is high under pressure loa