1. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Analysis of Sandwich Beams With a Compliant Core and With In-Plane Rigidity—Extended High-Order Sandwich Panel Theory Versus Elasticity
J. Appl. Mech. 2012;79(4): doi: /
Figure Legend:
Definition of the sandwich configuration

2. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Analysis of Sandwich Beams With a Compliant Core and With In-Plane Rigidity—Extended High-Order Sandwich Panel Theory Versus Elasticity
J. Appl. Mech. 2012;79(4): doi: /
Figure Legend:
Transverse displacement, w, at the top, z=c+f, for the case of graphite/epoxy faces and glass phenolic honeycomb core

3. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Analysis of Sandwich Beams With a Compliant Core and With In-Plane Rigidity—Extended High-Order Sandwich Panel Theory Versus Elasticity
J. Appl. Mech. 2012;79(4): doi: /
Figure Legend:
Through-thickness distribution in the core of the axial stress, σxx, at x=a/2 for the case of graphite/epoxy faces and glass phenolic honeycomb core

4. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Analysis of Sandwich Beams With a Compliant Core and With In-Plane Rigidity—Extended High-Order Sandwich Panel Theory Versus Elasticity
J. Appl. Mech. 2012;79(4): doi: /
Figure Legend:
Through-thickness distribution in the core of the transverse shear stress, τxz, at x=a/10 for the case of graphite/epoxy faces and glass phenolic honeycomb

5. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Analysis of Sandwich Beams With a Compliant Core and With In-Plane Rigidity—Extended High-Order Sandwich Panel Theory Versus Elasticity
J. Appl. Mech. 2012;79(4): doi: /
Figure Legend:
Through-thickness distribution in the core of the transverse shear stress, τxz, at x=a/10 for the case of E-glass/polyester faces and balsa wood core

6. Date of download: 11/2/2017
Copyright © ASME. All rights reserved.
From: Analysis of Sandwich Beams With a Compliant Core and With In-Plane Rigidity—Extended High-Order Sandwich Panel Theory Versus Elasticity
J. Appl. Mech. 2012;79(4): doi: /
Figure Legend:
Through-thickness distribution in the core of the transverse shear stress, τxz, at z=a/10 for the case of isotropic aluminum alloy faces and a wide range of isotropic cores