Test Results: Composite Panel Deflection & Stiffness

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The discussion focuses on discrepancies between test results and hand calculations for the deflection and stiffness of a composite panel under uniform pressure load. The user observed that hand equations yielded higher deflection values, leading to an unacceptable stiffness calculation. Participants suggest considering the theoretical background used for calculations, particularly if the panel consists of complex layered materials with orthotropic properties. There is a call for clarification on how stiffness values were derived and whether the testing method accurately reflects the panel's characteristics. Understanding the material properties and the calculation methods is crucial for resolving the discrepancies.
har_rai
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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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How did you come up with your values of stiffness and so? Was thinking whether the theoretical background you utilized is able to take account the properties of your panel, in case it's a more complex lamina/laminate (several layers which are orthotropic for example).
 
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