Date of download: 11/2/2017 Copyright © ASME. All rights reserved.

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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):041001-041001-11. doi:10.1115/1.4005550 Figure Legend: Definition of the sandwich configuration

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):041001-041001-11. doi:10.1115/1.4005550 Figure Legend: Transverse displacement, w, at the top, z=c+f, for the case of graphite/epoxy faces and glass phenolic honeycomb core

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):041001-041001-11. doi:10.1115/1.4005550 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

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):041001-041001-11. doi:10.1115/1.4005550 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

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):041001-041001-11. doi:10.1115/1.4005550 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

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):041001-041001-11. doi:10.1115/1.4005550 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