I will preface this thread, my ng900 is currently at sea level (where I've always lived) and now I'm moving to Montana 3800-6000ft avg.:lol: Okay so I've done my research and I realize there's pretty much two steps in turbo upgrades, IMO. Upgrading to a TD04-19t or a Big T-28 in the first step as a stock turbo upgrade. Or jumping to a gt2876, 2871, 3071, 3076, hx35, hx40, bigger turbos in general. Now I've done extensive research and calculations on the web, on saab central/saablink, and using T5 Suites features. I've found that when I do the calculations for a turbo at 5000ft above sea level the pressure ratio climbs dramatically and only larger frame turbos fit my flow requirements to make make power at elevation. Recently I stumbled upon this website that gives an engine flow rate calculator and will generate a graph for you to analyze what your engine needs so you can find a compressor map to fit it. This proved worthless when I discovered there was no adjustment for altitude. The I moved to the squirrel performance website where they give a calculator with all sorts of adjustment. What was key was their pressure reference for altitude changes. Now when using their website and doing my one calculations, I found that at ~5000ft above sea level (roughly 12.2psi Abs, remember ~14.7 at sea level) my pressure ratio to make even 18psi of boost was ~2.5. For 22psi boost, ~2.8. These ratios are easily past the capabilities of a stock t25 or 15t. Now to even hold these pressures for a mild upgraded turbo such as a 19t or a T28 they're pushing the limits of the T28 (IVE READ THAT A T28 CAN BE COMPARED TO THE GT28RS) but the 19t seems like it would fair better based on compressor map analysis. Using the Squirrel performance website I concluded that an upgraded turbo (19t/t28) would be needed to compare with upgraded t25 levels at sea level. Therefore to make more power (300+ range) I would need to upgrade immediately to say a 2876 to compensate for the elevation change.
The real thing I'm asking here is how turbos can cope with such extreme altitudes? It doesn't make sense that WRX's with such small turbos can even run 16psi at 5000ft?! When my t25 will barely be able to hold 18psi to 4000rpm. Most smaller frame garrett maps that Ive looked at max out at a pressure ratio a little over 3. Which at 5000ft will allow me 24psi MAX. I just want a turbo that will suffice around 300bhp but provide me room for improvement. Instead of buying the T28 upgrade and realizing I can only run 18psi because of the limits of the turbo at altitude.
I'm looking for experience with turbos at altitude. How'd you fair? What did you change? Was there specific tuning that you did so compensate? Did you skip the 19t/T28 jump and just go to a 2871 or 2876 instead?
The more info the better! Thanks so much!;ol; Please correct any of my data!
THIS LINK PROVIDES THE TURBO MAPS I'VE BEEN REFERENCING.
I've been reading a lot on this forum and most of the input is gold and supportive.
The real thing I'm asking here is how turbos can cope with such extreme altitudes? It doesn't make sense that WRX's with such small turbos can even run 16psi at 5000ft?! When my t25 will barely be able to hold 18psi to 4000rpm. Most smaller frame garrett maps that Ive looked at max out at a pressure ratio a little over 3. Which at 5000ft will allow me 24psi MAX. I just want a turbo that will suffice around 300bhp but provide me room for improvement. Instead of buying the T28 upgrade and realizing I can only run 18psi because of the limits of the turbo at altitude.
I'm looking for experience with turbos at altitude. How'd you fair? What did you change? Was there specific tuning that you did so compensate? Did you skip the 19t/T28 jump and just go to a 2871 or 2876 instead?
The more info the better! Thanks so much!;ol; Please correct any of my data!
THIS LINK PROVIDES THE TURBO MAPS I'VE BEEN REFERENCING.
I've been reading a lot on this forum and most of the input is gold and supportive.