Poisson's ratios are mechanical property values that indicate strain in a specific direction, caused by stress from another direction. These results are used in a subsequent Stress analysis.
To create these results, the Fiber orientation analysis if fiber material option must be selected, and a material with filler or fiber data must be chosen. This option can be found on the Fill+Pack Settings page of the Process Settings Wizard.
The Poisson’s ratio (averaged) (overmolding) result indicates the average strain in the second principal direction for the overmolded component, caused by the stress in the first principal direction.
The Poisson’s ratio (averaged) (overmolding) result is a fiber-over-thickness (FOT) averaged value, which means that the Poisson's ratio is calculated for every element on every laminate and then for each of those elements, it is averaged over all the laminates.
The Poisson's ratio (v12) (overmolding) result indicates the strain in the second principal direction for the overmolded component, caused by stress in the first principal direction. This result is laminate-based, recorded for each element on each laminate in the model, over the duration of the analysis. Thus, each laminate in the model will have a different result.
In general, vi,j=Poisson's ratio for transverse strain in the j-direction when stressed in the i-direction.
The Poisson's ratio (v13) (overmolding) result indicates the strain in the third principal direction for the overmolded component, caused by stress in the first principal direction. This result is laminate-based, recorded for each element on each laminate in the model, over the duration of the analysis. Thus, each laminate in the model will have a different result.
In general, vi,j=Poisson's ratio for transverse strain in the j-direction when stressed in the i-direction.
The Poisson's ratio (v23) (overmolding) result indicates the strain in the third principal direction for the overmolded component, caused by stress in the second principal direction. This result is laminate-based, recorded for each element on each laminate in the model, over the duration of the analysis. Thus, each laminate in the model will have a different result.
In general, vi,j=Poisson's ratio for transverse strain in the j-direction when stressed in the i-direction.
The thermo-mechanical property calculation for fiber-filled composites is based on the orthotropic assumption, that fiber-filled material properties are different in three orthogonal principal directions. Under this assumption, there are 9 independent mechanical constants and three independent thermal expansion coefficients. In models analysed using Midplane or Dual Domain analysis technologies, because of the plain stress assumption in the shell structure analysis in Warp, only 4 mechanical constants (tensile modulus in first/second principal directions, Poisson ratio v12, shear modulus G12) are necessary, and only these four are used in the (averaged) results.
Look at the Poisson's ratio (averaged) (overmolding) result to view the strain at a given point and compare it with the strain at other points on the model. The other results can be used for an more detailed study of the strain through the thickness.
For all but the Poisson’s ratio, (averaged) (overmolding) result, the results are laminate-based, so you can view the Poisson’s ratio distribution for each laminate in the model.
You can view the contour plot of a single laminate on the model, by clicking ( ). Select the Animation tab, and from the Animate result over drop-down list, select Single dataset.