A/R:
a small a/r means quick spool up time but the turbo will choke the exhaust at the higher rpms
a large a/r means a slow spool which equals lag but there is more potential for power in the high rpms.
a/r is determined by dividing the area of the turbine nozzle by the radius from the center of the turbine axle to the centroidof the housing throat.
Now on to the compressor maps:
pressure ratio(pr) is calculated by adding boost pressure(bp) and air pressure(ap), and then dividing the sum bye the air pressure. the equation would look like this:
bp+ap = pr
ap
lets say you are running 14 psi of boost at sea level and you want to find the pressure ratio, the equation would look like this:
14+14.7 = 1.95
14.7
so the pressure ratio is 1.95
now lets say you are running 14 psi at lets say 1000 feet above sea level. According to the book, you would subtrast .5psi for every 1000 feet above sea level you are. So the equation would look like this:
14+(14.7-.5)
(14.7-.5)
this simplifies down to this:
14+14.2 =1.98
14.2
so the pressure ratio is 1.98
the pressure ratio is shown on the verticle axis(the one going up and down on the left side) of compressor maps.
more in next post...
hopefully i explained this so everyone can understand it :)
This post has been edited by Apollorx7: 01 May 2005 - 06:04 PM

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