Hi,
For the simple tension test, the equation for a Mooney Rivlin material is as follows:
stress = 2*(C1+C2/stretch)*(stretch - 1/stretcth^2)
where
- stress is the engineering stress (force/original area)
- strain is the engineering strain (change in length/original length)
- stretch = 1+strain = length/original length
- C1 and C2 are the two constants. (In Fusion, these are A10 and A01.)
I assume that the fibers are small diameter, so I think it is impractical to model them and mesh them (using solid elements -- the only option in Fusion) as a separate part inside the hyperelastic. If this is true, then you are only going to model the dog bone, and the contribution of the fibers is assumed to be "present" in the measured material properties. (Maybe if the diameter of 1 fiber was 1/4 the thickness of the part, then it may be conceivable to model and mesh the individual fibers, and enter the material properties separately for the hyperelastic and the fiber.)
Also, the material models in Fusion assume that the properties are isotropic (the same in all directions). This may be reasonable if the fibers are randomly oriented throughout the volume. If the fibers are in some type of layup (like a composite would be), then the properties are orthotropic (different values in planes at 90 degree angles) or anisotropic (different in planes at some angle other than 90 degrees). I think that Fusion does not have orthotropic or anisotropic materials.
John Holtz, P.E. Global Product Support
Autodesk, Inc. If not provided, indicate the version of Inventor Nastran you are using.If the issue is related to a model, attach the model! See What files to provide when the model is needed.