http://www.turbosaturns.net/articles/turbo_compressor_maps_2.htmlthats another useful site.
This article all seems to revolve on density ratio...the power making formula. The formulas seem verry similar to what the TGP would run...but I don't know about the efficiency of the t25 on the tgp. I will try to plug in numbers latter with a supper 60 t3 just to see what happens...along with the stock IC....if any one can guess its cooling efficiancy.???
Air Temperature
Air temperature is an important variable because as the temperature increases the volume of air also increases. The following equation solves for ideal temperature rise, which is the temperature rise equivalent to the amount of work it takes to compress the air. Simply stated, the more you compress air (raise boost) the more the air becomes heated.
Equation
T2 = T1 (P2 / P1 )0.283
Variables
T2 = T1 (P2 / P1 )0.283 (Ideal turbo outlet temperture)
T1 = oF + 460 (Turbo inlet temperature)
P1 = 14.7psi (Turbo inlet pressure = 1 atm absolute)
P2 = P1 + desired boost (Turbo outlet pressure)
First, we need to solve for T1
T1 = oF + 460
In this example we will assume that the inlet temperature, which can also be interpreted as ambient temperature, is 80° F. Solving for T1 we get the following equation:
T1 = 80 + 460 = 540
Next, we need to solve for P2
P2 = P1 + desired boost
In this example we will assume a desired boost of 10psi.
24.7 = 14.7 + 10
The turbo's outlet pressure equals 24.7psi
We now have all the variables needed to solve for T2.
T2 = T1 (P2 / P1 )0.283
Variables
T1 = 540
P1 = 14.7
P2 = 24.7
Solving for T2
T2 = 540 (24.7 / 14.7 )0.283 = 625.43
Then take the answer for T2 and subtract 460 from it
625.43 – 460 = 165.43° F
The ideal turbo outlet temperature equals 165.43° F, which is a raise in temperature of 85.43° F over the assumed starting inlet temperature of 80° F. Giving us a ideal outlet temperature rise of 85.43° F. (165.43 – 80 = 85.43)
Adiabatic Efficiency
We have solved for the ideal outlet temperature of the turbo, which assumes 100% adiabatic efficiency (AE). At 100% AE there is no loss or gain of heat from the turbine but in the real world AE's normally run between 60-75% and we need to compensate for this. The following equation allows us to compensate for a less than perfect AE.
Ideal Outlet Temperature Rise / AE = Actual Outlet Temperature Rise
The basic plots diagramed in the previous article Deciphering turbo compressor maps gives us a good idea of which efficiencies the turbo will spend most of it’s time. In the image below we see two points located within the 74% range and one point in the 70% range. I decided to take the average of the three points (74 + 74 + 70 / 3 = 73) and use that as my compensated AE value. If we assume that the compressor has an AE of 73% then the outlet temperature will be 27% higher than the ideal outlet temperature (100 – 73 = 27). Again the equation is:
Ideal Outlet Temperature Rise / AE = Actual Outlet Temperature Rise
Substituting our numbers in we get:
85.43 / .73 = 117.02° F
117.02° F is the Actual Outlet Temperature Rise, which once added to the inlet temperature (80° F) gives us the actual outlet temperature.
80 + 117.02 = 197.02° F
197.02° F is the actual outlet temperature of the turbo without using an intercooler.
Air Density Ratio
Air temperature and adiabatic efficiency have a profound effect on the air density ratio.
As the air is heated it expands, increasing its volume, but becoming less dense. The formula for solving the air's density ratio is located below.
(T1 / [T1 + Actual Outlet Temperature Rise]) x (P2 / P1) = Air Density Ratio
Plugging our numbers into the formula we get:
(540 / [540 + 197.02]) x (24.7 / 14.7) = Air Density Ratio
Stepping through the math:
(540 / 737.02) x (24.7 / 14.7) = 1.23
1.23 is the Air Density Ratio
To find out the difference in volume the heated air makes we need to compare the turbo's inlet airflow with the outlet airflow. Taking all of the variables into account we will now be able to find the turbo's actual outlet airflow in CFM by using the following equation.
Turbo Outlet CFM* x Density Ratio = Actual Outlet CFM
171.16 x 1.23 = 210.53 CFM
Outlet CFM* is the value taken from the article Deciphering turbo compressor maps.
Reviewing the first article Deciphering turbo compressor maps we see that the value of 19.84 lbs/min was given for an engine running 10psi of boost without correcting for any variables. Using the corrected formula above we find that the same 10psi yields 14.53 lbs/min, which represents a difference of 27%. This is a sizable drop in airflow from theoretical (the first article) to the more accurate (this article).
Nevertheless, the key to finding the turbo best suited for your application is to make sure that the airflow and pressure ratios intersect at a flow value no less than 60%. Also, there will most likely be several compressor maps that fit your application if this is the case it is advisable that you pick the compressor that has the lowest surge air flow limit. This will insure that you have the widest range of performance at that boost. Armed with this additional information you should be able to better calculate your turbo’s actual airflow numbers.
*Boost pressure will be the absolute value, which is 1+ what you are boosting. For example if your are boosting .7 bar add a 1 before you insert the value into the equation. By adding 1 you are compensating for the 1 bar of standard atmosphere pre-boost.
Converting CFM to lbs/min
210.53 x 0.069 = 14.53
Also on the WBO2...the box I was reffering to was the unit itself you made...that I need a pc board for. You know....with the stock O2 or Limbada "spelling" O2...the A/F meter and ecm plug into it directly...with nothing in between....but with a WBO2...you need a box.
And boost cut eliminator....the easyest is reprogramming your chip..I raised mine to 14.3. almost max for the 2bar...other methods are verry crude to your engine. I've also eliminated boost cut on top speed and top speed itself. With chip programming...you can even run more timming for race gas or adjust timming for traction out of the hole. I'm just about ready to try my chip.