telnar1236
Master member
The EDF I'm using already has the stator vanes built in so fortunately no real need to add them in myself. Out of curiosity, what's your thinking behind using the NACA 0006 airfoil instead of a cambered airfoil?Now that you found a increase for the tail cone, I am going to suggest you look at putting at least 4 stator vanes for a better increase of least 6-10% thrust gain. This allows the flow to changing rotational into linear axial flow for better thrust. You should use a NACA 006 airfoil(taper trailing edge to a point) and stay between 5 to 10 degrees for incidence angle. Over ten degrees will reduce top speed.
So here is tail cone with the built into 4 stator vanes that gave the 6 bladed EDF plenty of power
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In design, one other factor that I played with is reducing the tip gap between the blades and outer wall. I used Scotch magic tape (2 layers of tape .010-.015) and it increases the internal pressure of the duct as well as reducing spillage back into the entrance of the EDF so the thrust increases 4-6% more.
Imagined 3d printing a thin ring and putting that in between the blades and housing. Remember that the blades lengthen when spinning, so leave some small gap(less than 1 % of the blade tip chord) otherwise you will loose 3% thrust due to interaction between rotor tip and duct wall.
View attachment 258206
Think I'm a bit too scared of the tape getting tangled up in my expensive 80mm 6s unit to try that trick on this plane, but I do need to try it sometime - 4-6% more thrust is always welcome