Compressor Inlet Conditions
•
Stagnation Temperature
•
T
02
=T
a
(1+M
2
(k-1)/2)
•
•
Stagnation Pressure
•
P
02
=p
a
(1+n
d
(T
02
/T
a
)-1))
k
d
/(k
d
-1)
•
n
d
=adiabatic diffuser efficiency