AbstractThe aim of this article is to investigate the effect of a kind of polymer foam and skin on bending behavior of open cell polymer foam based sandwich structures using three point flexural tests. The flexural test has core shear stress, face sheet bending stress and also beam deflections were considered for studying bending behaviour of the sandwich structure. The results show the polymer-polymer cored-polymer(PPP) sandwich has maximum bending strength compared to other five sandwich structures. Failure mechanisms of the fractures specimen were studied through scanning electron microscopy, which reveals that delamination starts at interface between core and skin of the sandwich structure though initiated at the middle of the polymer c...
Polymethacrylimide (PMI) foams have been widely applied in aerospace engineering as the core materia...
Polymethacrylimide (PMI) foams have been widely applied in aerospace engineering as the core materia...
Debonding between the skins and the core in a sandwich structure is a critical failure mode in autom...
Sandwich structures offer innovative alternative solutions to many weight-critical industrial fields...
While the polymeric foam cored sandwiches have been realized for many years, recently there is a gro...
As a light structure, composite sandwich panels are distinguished by their significant bending stiff...
This paper addresses the flexural properties of sandwich structures with cellular core materials. Ex...
A recently developed glass fibre reinforced PU-foam sandwich panel is mechanically characterized in ...
A recently developed glass fibre reinforced PU-foam sandwich panel is mechanically characterized in ...
This paper deals with the mechanical investigation of 3-D reinforced CFRP foamcore sandwich structur...
This study presents the main results of an experimental, theoretical and numerical investigation on ...
In this paper, the bending stiffness-to-weight-ratio of novel hybrid sandwich structures is investig...
Polymethacrylimide (PMI) foams have been widely applied in aerospace engineering as the core materia...
Polymethacrylimide (PMI) foams have been widely applied in aerospace engineering as the core materia...
Polymethacrylimide (PMI) foams have been widely applied in aerospace engineering as the core materia...
Polymethacrylimide (PMI) foams have been widely applied in aerospace engineering as the core materia...
Polymethacrylimide (PMI) foams have been widely applied in aerospace engineering as the core materia...
Debonding between the skins and the core in a sandwich structure is a critical failure mode in autom...
Sandwich structures offer innovative alternative solutions to many weight-critical industrial fields...
While the polymeric foam cored sandwiches have been realized for many years, recently there is a gro...
As a light structure, composite sandwich panels are distinguished by their significant bending stiff...
This paper addresses the flexural properties of sandwich structures with cellular core materials. Ex...
A recently developed glass fibre reinforced PU-foam sandwich panel is mechanically characterized in ...
A recently developed glass fibre reinforced PU-foam sandwich panel is mechanically characterized in ...
This paper deals with the mechanical investigation of 3-D reinforced CFRP foamcore sandwich structur...
This study presents the main results of an experimental, theoretical and numerical investigation on ...
In this paper, the bending stiffness-to-weight-ratio of novel hybrid sandwich structures is investig...
Polymethacrylimide (PMI) foams have been widely applied in aerospace engineering as the core materia...
Polymethacrylimide (PMI) foams have been widely applied in aerospace engineering as the core materia...
Polymethacrylimide (PMI) foams have been widely applied in aerospace engineering as the core materia...
Polymethacrylimide (PMI) foams have been widely applied in aerospace engineering as the core materia...
Polymethacrylimide (PMI) foams have been widely applied in aerospace engineering as the core materia...
Debonding between the skins and the core in a sandwich structure is a critical failure mode in autom...