Thermodynamics

Gas Compressor Power Calculator

Single-stage adiabatic compression power, head, and discharge temperature for an ideal gas.

H_ad = Z R T₁/M · k/(k−1) · [(P₂/P₁)^((k−1)/k) − 1]; P = ṁ H_ad / η

How it works

For an ideal gas compressed adiabatically, the head depends only on suction temperature, pressure ratio, and the gas properties k and M. Multiplying by mass flow gives gas power; dividing by isentropic efficiency gives shaft power and an estimate of the actual discharge temperature.

Worked example

1000 kg/h of air from atmospheric pressure to 5 bar abs at 75% isentropic efficiency. ≈ 65 kW of shaft power, with discharge around 200 °C ideal — hot enough that real machines intercool at this ratio.

Inputs

Frequently asked questions

Why is my discharge temperature so high?

Adiabatic compression converts work into internal energy: T₂ = T₁·r^((k−1)/k). At a ratio of 5 with air that is already ~200 °C ideal, and inefficiency makes it hotter. This is why multi-stage machines intercool between stages.

When do I need multiple stages?

Common practice keeps the ratio per stage around 3–4, limited by discharge temperature (seals, lubricants, materials) and efficiency. The tool flags ratios above 4.

Is this valid for real (non-ideal) gases?

Approximately, via the average compressibility factor Z. For high pressures, gas mixtures near their dewpoint, or CO₂-rich streams, use an equation-of-state simulation — the ideal-gas path deviates significantly.

Assumptions

References

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