While this seems like a fairly straightforward question, and it can be calculated, the complex geometry of the impeller (even if exact geometry is known) makes the calcs challenging.
Remembering that water is incompressible (neglecting any entrained gasses) simplifies the calcs of a waterjet pump vs. a similar gasjet pump (like an aircraft jet engine).
Having said that, the basic equation set to use, the
Reynolds-averaged Navier–Stokes equations (or
RANS equations)
http://en.wikipedia.org/wiki/Reynolds-averaged_Navier–Stokes_equations, is intimidating:
View attachment 18591
Description of the method to use RANS:
View attachment 18592
View attachment 18593
This can be simplified by using a graphical approach as described here:
http://www.wseas.us/e-library/conferences/2006venice/papers/539-661.pdf
PS: Just kidding - these calcs are possible, but obviously not for most people.
A far better idea would be to go to Yamaha or other source that has empirically tested flow rate. Good luck in your quest, young Jedi.
Note: I did some work like this in engineering school but that was a long, long time ago in a galaxy far, far away.
Protip: Never take a course from a Thermodynamics II professor whose research area is shockwave modeling at the tip of a supersonic impeller.