Exit Temperature of an Isentropic Compressor
Air enters a compressor at and , and is compressed isentropically to .
Treat air as an ideal gas with constant specific heat ratio .
Find the exit temperature .
| P1 | 100 kPa | Inlet pressure |
| T1 | 300 K | Inlet temperature |
| P2 | 800 kPa | Exit pressure |
| k | 1.4 - | Specific heat ratio |
Hint 1
Isentropic means constant entropy — there is a standard P-T relation for an ideal gas.
Hint 2
T₂/T₁ = (P₂/P₁)^((k−1)/k). The exponent is the part most people get wrong.
Hint 3
(k−1)/k = 0.4/1.4 ≈ 0.286, not 3.5.
Worked solution — try the problem first
For an ideal gas undergoing an isentropic process with constant :
Exponent:
Pressure ratio:
Because this is a ratio, the kPa units cancel — no need to convert to absolute pressure units, though both must be absolute pressures (they are).
Sanity check: compression must raise temperature, and it does — by roughly 243 K. An answer below 300 K would be non-physical.
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