I'll one up Rob's map, and I'll map out the pressure ratios on a t04e 60trim, that a 5m turbo will consume at ~350hp. The first map is at sea level, the second is at ~14k feet, or .6 atmospheres, as Rob has has used in his explaination. Temperatures are static, and I've not compensated for the effect of reduced pressure at the tailpipe on spool speed.
Your "holy-crap-batman-surging" 60-trim at 14k feet says otherewise...
HAC also compensates for turbo efficiency, don't forget it.
Enjoy,
--billyM
figgie;1097354 said:Actually, the only thing that really has changed at sea level v. the 1+ atmosphere inside of your manifold is absolute pressure.
Barometric compensation - compensates for the density due to altitude if you use it that is. If you do use it, it helps in adjusting for changing exhaust velocity due to the lack of atmosphere hindering the exhaust on it's way out.
Hence why turbo props can go to 20k+ feet and still remain running.
300kpa inside of your manifold stays the same if it is 300kpa @ sea level or 300kpa @ 30k feet.
Your "holy-crap-batman-surging" 60-trim at 14k feet says otherewise...
HAC also compensates for turbo efficiency, don't forget it.
Enjoy,
--billyM
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