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## Homework Statement

Most sandwich panels are made up of two face sheets and a core. The core is often light, weak and

contributes very little to the stiffness of the panel. This enables a very rough analysis to be made by

assuming that the core is just air and that the cross‐section of the panel is equivalent to a rectangular crosssection tube. Using this assumption derive an equation for

*E*~ in terms of the outer dimensions of the panel (

*b>>h*) and the value of

*E*for the face material. Hint: equate equations 1 and 2 for the same values of span,deflection, force and

*C1*and note that because

*b>>h*the rectangular tube second moment of area can be given as

*I*~

*h*2

*tb*/ 2 . Note that you are not calculating a value here, just finding an expression in terms of the aforementioned variables.

Use the assumption in the previous point to derive an approximate equation for the effective density, ρeff , of the panel. Hint: start by assuming the panel is

*b x b x h*in size and calculate the volume of material in the two face sheets of thickness

*t*(you can ignore the side strips). Your equation will be in terms of

*t/h*.

Use your equations to estimate the effective stiffness of a wood (parallel direction) face‐sheet sandwich

panel (with a negligible weak light foam core). Assume the panel apparent density is 50 kg/m3. Comment on whether the result falls in the ‘desired’ region of property space in Figure 1.

## Homework Equations

s= (L^3*F)/C*E*I and s=(L^3*F)/C*Eeff*Iouter

Area box tube( neglecting sides) 2*t*b, Volume bt = 2*t*b^2

## The Attempt at a Solution

Assuming L, F,S and C are the same we are left with E*I=Eeff*Iouter

E*(h^2*t*b)/12=Eeff*(b*h^3/12)

Eeff/E = 6t/h

ρ=mass/volume

ρeff=m/b*b*h and ρ=m/2*t*b^2

m= ρeff*b^2*h=ρ*2*t*b^2

ρeff= 2ρ*t/h

50=2*ρ*t/h

I think I have derived the equations correctly except for the E and the ρ stop the equation being used to find the desired values.

Thanks in advance for any help.