I'm starting a new project with two brand new Garrett GT2560R turbos coming my way as we speak ...

The goal with this project is to build a "Low Cost - Free Turbine" gas turbine concept, a bit like a PT6, but much smaller and much cheaper and see how much HP and/or torque can I get out of this "Pair", one driving the other.
For this, I'm planing to use the good and "Reliable" John Wallis flame holder hole area calculation based on the turbine "Inlet" area and NOT the compressor inlet area like Springer would suggest.
Now, I heared dealing with pretty small turbos can be a pain in the (You know what), thus, I'm asking here before spending thousand of $$$ in parts ... "Any comments and/or suggestions and/or warnings before I start???"
And as for the "Ejector" modeling and CFD analysis John, I'm now pretty close to the best results I can draw from this one with only 1 or 2 CFD to do, and I'm now up to 1.36 lbs/sec sucked out that cabinet ... That's ALOT of air for such a small ejector gap ...

Thanks and cheers to you all guys ...
