nasa / CompDam_DGD

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Under longitudinal compression and shear, matrix damage due to shear may not occur #13

Open acbergan opened 5 years ago

acbergan commented 5 years ago

The model is implement so that only one damage mode (fiber tension, fiber compression, or matrix damage) is activate at each integration point. Under combined stress cases, the first failure criteria to be satisfied determine which damage mode is activated.

When the following conditions are satisfied, matrix damage will not occur when it would be expected:

A work around for this issue in structural models is to use the alternating section definition method (Hyder et al, 2018) with the strips of elements designated for matrix cracking having the fiber kinking model disabled.

Fundamentally, a better understanding of the material behavior under combined longitudinal compression and shear is needed.