I was putting this together to find out if the turbo I have is going to be too small for my goals, maybe this will help some of you guys out also...
__________________________________
:::: Engine Airflow Requirements :::
__________________________________
(CID × RPM) ÷3456 = CFM
CFM × 0.85 = CFM @85%VE
----------------
__________________________________
:::::::::: pressure ratio ::::::::::
__________________________________
(psi + 14.7) ÷ 14.7 = pressure ratio
----------------
__________________________________
:::::: Temperature rise ::::::::::::
__________________________________
T2 = T1 (P2 ÷ P1)^0.283
Where:
T2 = Outlet Temperature °R
T1 = Inlet Temperature °R
°R = °F + 460
P1 = Inlet Pressure Absolute
P2 = Outlet Pressure Absolute
T1 = temp°F + 460 = °R
P2 = 14.7 + psi = psi
°R - 460 = °F Ideal Outlet Temperature
----------------
__________________________________
:::::::: Adiabatic Efficiency ::::::
__________________________________
(ideal outlet temp - inlet temp) ÷ 0.7 =°F Actual Outlet Temperature Rise
temp + actual rise = °F Actual Outlet Temperature
----------------
__________________________________
::::::::: Density Ratio ::::::::::::
(Inlet °R ÷ Outlet °R) × (Outlet Pressure ÷ Inlet Pressure) = Density Ratio
----------------
__________________________________
::: Compressor Inlet Airflow ::::::
__________________________________
Outlet CFM × Density Ratio = Actual Inlet CFM
CFM × 0.069 = lbs/min
----------------
HERE'S WHAT I CAME UP WITH
__________________________________
:::: Engine Airflow Requirements :::
__________________________________
(98 × 6600) ÷3456 = 187.15 CFM
187.15 × 0.85 = 159.08 CFM @85%VE
----------------
__________________________________
:::::::::: pressure ratio ::::::::::
__________________________________
(15 + 14.7) ÷ 14.7 = 2.02 pressure ratio
----------------
__________________________________
:::::: Temperature rise ::::::::::::
__________________________________
T2 = T1 (P2 ÷ P1)^0.283
Where:
T2 = Outlet Temperature °R
T1 = Inlet Temperature °R
°R = °F + 460
P1 = Inlet Pressure Absolute
P2 = Outlet Pressure Absolute
T1 = 75°F + 460 = 535°R
P2 = 14.7 + 15 = 29.7psi
T1 = 535
P1 = 14.7
P2 = 29.7
T2 = 535 * (29.7 ÷ 14.7)^0.283 = 652°R
652°R - 460 = 192°F Ideal Outlet Temperature
----------------
__________________________________
:::::::: Adiabatic Efficiency ::::::
__________________________________
117 ÷ 0.7 = 167.14°F Actual Outlet Temperature Rise
75 + 167.14 = 242.14°F Actual Outlet Temperature
----------------
__________________________________
::::::::: Density Ratio ::::::::::::
(535°R ÷ 652°R) × (29.7 ÷ 14.7) = 1.66 Density Ratio
----------------
__________________________________
::: Compressor Inlet Airflow ::::::
__________________________________
159.08 × 1.66 = 264.07 Actual Inlet CFM
264.07 × 0.069 = 18.22lbs/min
----------------
let's take a look at how this all adds up, here is a compressor map for the T3 "40" trim

2.02 pressure ratio
18.22lbs/min
if you intersect the lines it lands outside its efficiency range
this shows that when the engine is hitting peak HP @ 15psi the turbo will be operating outside of it's efficiency range, so you will need to go bigger with the turbo, in this case the T3 "50 trim" would be perfect
