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Altitude: 50-80 and 30-90


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Something interesting for you altitude folks that are doing this...

 

IF your MAF is scaled relatively close to reality, the folks in Denver (12.2 psi roughly) can take their airflow and multipy it by 1.23 to see how many g/s they would be flowing at sea level with the same volumetric amount of air...

 

260 g/s is roughly 320 g/s...

 

The calculation is based on a 70 degree day, but does not change much with temperature...

 

For C-springs where I log (11.42 psi) it is A 1.315 multiplier ;) (260 converts to 342 g/s)

 

This is not a true conversion as in most cases you would be outside the efficiency of your compressor, or off the map completely (i.e. you can't go there) if you did this exact thing. Pretty cool anyway :D

:spin:
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  • 7 months later...
I'm also at a fairly high altitude (Salt Lake City about 4,400ft). I'm finding my typical 60-80 runs in the low to mid 3's and high 4's for my 50-80. I only have an STI up and my first cat gutted after my turbo. I'm still tweaking my tune, but I was wondering if Airboy's spreadsheet is close to actual rear wheel HP numbers? I'm about 230hp and 260tq. Thanks for any feedback.
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