GT3071RWG 56.5mm turbine T25 flange in a .86AR flows 24lbs corrected turbine gas flow.
GT3076r 60mm turbine T3 flange in a .82AR flows about 23lbs.
It looks like the smaller T25 style GT3071r would definitely have less backpressure. The turbine is also smaller on this varient of the 3071r. It is a smaller 56.5mm turbine in the same 84 trim as the GT3076R 60mm.
Even with the larger turbine, the .82 still doesn't flow what the smaller GT3071r internally wastegated .86 does.
I would just love to see what this housing flows, but I have the feeling it is going to be about 15-18.
Now, I also know that the divided housing will help prevent reversion, which is why I figured it would work really well. But the backpressure from the housing just
feels like it is not responding really well. Now that the log is gone, the standard cams can be used, but they still don't want to make power. The VE cams hit hard when the ex hits, so does that mean there is more exhaust restriction?
The .78 if it really flows like .39 (like a very respected DSM guy is telling me) it would really choke the engine. The great spool comes at a very steep price, but you could just say "F* the twin scroll" and get a 2871r or something that just spools better. There is only half as much gas that has to pass through each scroll, but here's where it gets a little confusing. You could have a turbo with 4 scrolls, but if each pulse had to go through a hole smaller than the exhaust port it would create a loss of power right? That's what I am thinking is going on. Since the gas doesn't flow through the turbine all at once, but goes in pulses, each pulse basically goes through a hole the size of a dime in the volute. Each pulse goes through its own .39 housing. Does that make sense at all?
Maybe it just needs 30psi of boost eh? Race gas and tons of timing. That should make good power