Abstract—At present the study of mechanical properties of new quasi-honeycomb sandwich structure’s core research, ignored the thickness of quasi-honeycomb cell wall,that is, when establish finite element model of the structure, pick up the same thickness of quasi-honeycomb cell wall of modeling; While in practice, the hexagonal hypotenuse of the quasi-honeycomb unit cell should be double. In response to this problem, in consideration of the unit cell thickness conditions, re-derive the effective elastic constants of new quasi-honeycomb sandwich structure’s core and compared with those of hexagonal honeycomb sandwich structure, and the results show that both equivalent elastic moduli are approximately equal, but the quasi-honeycomb sandwich ...
Aiming at a complex polygonal honeycomb structure,using the virtual work principle,the analytic form...
In the aeronautical field, sandwich structures are widely used for secondary structures like flaps o...
Numerical modeling of honeycomb structures in aerospace engineering is too tedious and time consumin...
ABSTRACT: Different detailed finite element model alternatives are developed to come up with the mos...
The honeycomb core model was built by finite element method( FEM). And based on Hooke ’s law,the equ...
Sandwich structures are widely used in many technical applications, because their composition combin...
ABSTRACT: Analytical expressions for the effective elastic properties of cellular hexagonal honeycom...
This work deals with the influence of geometry on the equivalent transverse shear stiffness of honey...
AbstractIntroducing hierarchy into structures has been credited with improving elastic properties an...
The paper proposes first to study the behavior of honeycomb alone under uniform cyclic compression-r...
This report presents a numerical analysis of three-dimensional mechanical properties of metallic ho...
The influence of the nine orthotropic material properties of honeycomb on the dynamic response of a ...
ii Honeycomb structures are widely used in many areas for their material characteristics such as hig...
A computational homogenization technique (CHT) based on the finite element method (FEM) is discussed...
Honeycomb sandwich core is typically modeled as an equivalent continuum for both static and dynamic ...
Aiming at a complex polygonal honeycomb structure,using the virtual work principle,the analytic form...
In the aeronautical field, sandwich structures are widely used for secondary structures like flaps o...
Numerical modeling of honeycomb structures in aerospace engineering is too tedious and time consumin...
ABSTRACT: Different detailed finite element model alternatives are developed to come up with the mos...
The honeycomb core model was built by finite element method( FEM). And based on Hooke ’s law,the equ...
Sandwich structures are widely used in many technical applications, because their composition combin...
ABSTRACT: Analytical expressions for the effective elastic properties of cellular hexagonal honeycom...
This work deals with the influence of geometry on the equivalent transverse shear stiffness of honey...
AbstractIntroducing hierarchy into structures has been credited with improving elastic properties an...
The paper proposes first to study the behavior of honeycomb alone under uniform cyclic compression-r...
This report presents a numerical analysis of three-dimensional mechanical properties of metallic ho...
The influence of the nine orthotropic material properties of honeycomb on the dynamic response of a ...
ii Honeycomb structures are widely used in many areas for their material characteristics such as hig...
A computational homogenization technique (CHT) based on the finite element method (FEM) is discussed...
Honeycomb sandwich core is typically modeled as an equivalent continuum for both static and dynamic ...
Aiming at a complex polygonal honeycomb structure,using the virtual work principle,the analytic form...
In the aeronautical field, sandwich structures are widely used for secondary structures like flaps o...
Numerical modeling of honeycomb structures in aerospace engineering is too tedious and time consumin...