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Honeycomb panel test

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ghfjdkjlhk

Mining
Sep 28, 2008
1
Hi:

Recentlly we tested a composite panel for uniform pressure load and tablulated the deflection at few location where we were intersted.But when I tried to use hand equations to calculate the stiffness/deflection and I got totally diffefrent results for deflection.Actually deflections are more in hand eqations.

Now am I wondering which deflection to use to calculate stiffness.

If I use from hand results, stiffness (total load from pressure /deflection)is not acceptable because sfiffness is small than required.

Can anyone tell what I am missing?

Thanks in adwanse.
 
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Did you take in account the shear deflection? for an honeycomb panel isn't negligible.
Onda
 
Hexcel published some technical papers dealing with the strength and deflection of composite structures. If you are using such a structure (metallic skins glued to a hex-cell core), they can help.
 
What boundary conditions were used for the test panel?
How was the load applied?
What boundary conditions were used in your analysis?
Is it a constant thickness panel, or do the facesheets ramp down into a laminate edgeband?
Have you included transverse shear deflection in your analysis?
 
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