In: Mechanical Engineering
Derive the flexural rigidity of a sandwich beam whose breadth is b, which has a core of thickness c and skins of thickness t each. The distance between the centroids of the skins is d, the skin and core moduli are Es and Ec respectively.
To derive the flexural rigidity of a sandwhich beam,
breadth = b
Core of thickness = c
skin of thickness = t
the distance between the centroids of the skins is = d
skin and core moduli are Es and Ec respectively
total thickness of the sandwich is d = c + 2t
The equivalent flexural rigidity (EI)eq can be write as the sum of the flexural rigidity of the core and of the two faces.
(EI)eq = Ec Ic + 2 Es Is
Where I is Moment of Inertia
By using parallel axis theorem
(EI)eq = ( Ec b c3 ) / 12 + Es [( b t3 ) / 6 + ( b t d2 ) / 2 ]
assumes that the skin’s thickness t is very much thinner than the thickness of the core c and that the Young’s modulus of the core is at least an order of magnitude smaller than that of the skins, the equation can be simplified as follows
Equivalent flexural rigidity (EI)eq = Es (b t d2 ) / 2 .