Composite Sandwich Panel Bending Stiffness & Deflection Calculator - Simple Supported
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Umut Aksoy
Composite Sandwich Panel Stress Calculator
24 March 2017
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This is the Composite Sandwich Panel (Simple Supported) Bending Stress, Core Stress, Ply(skin) Stress, Stiffness & Deflection Calculator - Simply enter the values to calculate the design parameters of the composite sandwich panel.
P (lbs)
=
tc (inch)
=
tf (inch)
=
Ef (psi)
=
b (inch)
=
L (inch)
=
Gc (psi)
=
P is the applied load on the panel.
tc is the composite panel core thickness.
tf is the composite panel skin(ply) thickness.
Ef is the elasticity modules of the skin.
b is the width of the panel.
L is the distance between supports.
Gc is the shear modules of the core. If you don't know the shear modules of the core leave it blank.