The moment of inertia of a propellar would be fairly easy to calculate, you'd just calculate the moment of inertia of one of the propellar arms and then times that by the number of arms there are that make up the propellar. The propellar arm could be modelled as a thin uniform rod being rotated about its end and I'm sure wikipedia will have a full table of moments of inertia for such constructions. You can even calculate it if your handy with maths:
I=∫r2dm;dm=μdr I=μ∫0Lr2dr=3μL3
M=μL→I=31ML2
So total I would be I=3NML2 if the propellar had N arms.