I had a close look at my GT turbine wheel today. The outside edges of the wheel are 100% perpendicular, but when looking a certain angles, can have the illusion that one edge is longer.
Now looking at the shape of the volutes in the pic below, it appears that if one port was closed, the gas would push out at an angle, correct? It looks like gas coming strictly out of the left volute would have more momentum towards the downpipe outlet, whereas the right volute would push more towards the CHRA. If this is true, and assuming we are trying extract more rotational energy from a low volume of fast moving gas, which would be more effective? Perhaps closing the port closest to the CHRA would have the gas firing at a more forceful direct/perpendicular angle against the outside edges of the turbine? The gas would have to make a sharper turn to flow out of the turbo, which would be bad for flow, but could be best for harnessing that extra gas speed the SP valve is providing. If the turbine has more resistance to flow that should translate into faster spool using the right volute compared to the left.