RE: HELP! propeller ducting question
If the purpose of the duct is to reduce losses between vortex sheets (to approximate an infinite number of blades), that 1/2 inch clearance at the tips needs to be reduced to absolute minimums (1/8" maybe?). And even then, under static conditions, the benefits are almost non-existent. The difference shows up at high advance ratios according to Prandtl's effective diameter theory.