Hi Barrie,
Michael pointed out a big issue with your model. If I was in your shoes I would try recreating the blade so that the le is smooth. Also, you want to have a circular arc trailing edge. What I have been doing is making a solid blade and a solid hub or spinner in your case. Then boolean those. Then I check to make sure it is one solid. If you get that far, you can then fillet the edge. I have found Rhino and MoI to be very hit and miss with these things. One thing that seems to be a problem is if there is a seam in this area. I usually have to rotate the hub/spinner so the seam for that part is not in the area you want to fillet. I don't know why this is an issue, perhaps Michael can shed light on it. Lastly, you can experiment with the fillet radius. Usually your te radius will limit the size of the fillet you can put at the root of the blade. So if you want a really big fillet you will have to increase the te radius. You can get this to work, but it is frustrating and takes a lot of trial and error. What I wrote above, is what I have learned with battling with this type of thing for a long time. In Rhino I check the validity of the solid by calculating volume for it. If Rhino fails to calculate a volume for each part, chances are the fillet operation won't work. Also, the final solid (before filleting) should be able to calculate a volume. If not, Rhino would fail to fillet. MoI doesn't have that ability. But from what I saw in one of Michael's recent posts, it looks like volume calculation is coming with v4. However, I don't know if this is a good indicator of fillet success for MoI (as I haven't played with the v4 beta).
Also, many years ago a forum user here named Burrman figured out the NACA airfoil leading edges are elliptical. So if you use the elliptical curve tool to create the le, that will get you the correct airfoil le. I've never had any issue with the fillet failing at the le using this technique. Which burrman taught me here, ages ago. The suction and pressure curves of the airfoils I create using the NACA definition. Never had issues there either. Usually the failure happens around the te because you want a root fillet that is bigger than geometrically possible to create or if there is a model seam in the root fillet area. Any other issue has been because of subtlety corrupt geometry (like Michael pointed out with your model). I've had many models not get created the way I thought and had to redo them, so you're not alone. Usually, the calculate volume trick tells me if the model is good or not. This is because, for me at least, whatever is wrong with the model you can't really see most of the time. Sometimes, I have to just abandoned whatever method I tried to make the blade, and go with a different approach. After years of doing these models, I found just using a loft of various airfoil shapes was the best way. Otherwise, rhino would screw it up. Doing a loft is about the only sure fire way of getting the exact blade shape right. I usually use 13 airfoils along the blade. I position them where they are supposed to be and then loft it. If you have the ellipse at the le and the arc at the te everything should work out. You end up having to redo it all if you aren't happy with the size of the root fillet that you can generate.
Anthony
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