What makes static thrust, especially with its relationship to propellers, is, as several people have already pointed out, a tricky business. If you are only interested in how short a takeoff roll you might need for takeoff, then the prop with the largest static thrust is probably a good indicator (depends a little on how much airspeed you need to lift off!).
When you are holding the plane, the propeller is biting into the air at more or less its stated pitch (~angle of attack). Once the plane is moving, the angle of attack decreases due to the forward component of the relative airspeed. In straight and level flight, the plane is no longer accelerating (tangentially at least!) so at that point, the thrust just equals the drag (F=ma, with F= Thrust-Drag, m=mass, a=acceleration=0 at cruise). At this point the prop you chose for maximum static thrust may be flying you too slow in the air.
Since you are never flying at zero airspeed during the pattern (ignoring Bi-Slobs!), the zero speed prop choice most likely won't be the best choice in the air. My own GUESS, is that the best prop, for a given engine is one that provides the best thrust at the lowest airspeed of the pattern. I am also guessing this is somewhere in the vertical climb after a square corner. That prop will keep the plane accelerating the best(or from decelerating the least) and thus have the best line tension. At this stage as far as I know, this will be an empirical excercise with lots of prop selections if you are using <$5 props.
I believe Al Rabe may have made measurements with motors mounted on a moving car (at least I think he did for wings). A working man's version of a wind tunnel.
My 2 cents!