Model compression and expansion with a polytropic law. Switch between known states and unknown properties. Get work, heat estimate, and plots-ready exports instantly here.
| Case | P1 (kPa) | V1 (m³) | T1 (K) | n | Known | Value | Computed (P2, V2, T2) |
|---|---|---|---|---|---|---|---|
| A | 200 | 0.050 | 300 | 1.30 | P2 | 500 kPa | V2 ≈ 0.0260 m³, T2 ≈ 390 K |
| B | 150 | 0.030 | 320 | 1.00 | V2 | 0.060 m³ | P2 ≈ 75 kPa, T2 ≈ 320 K |
| C | 400 | 0.010 | 350 | 1.20 | T2 | 450 K | P2 and V2 from T·V^(n−1) |
A polytropic process follows P·Vn = C, where the exponent n models heat exchange and irreversibilities in a compact way. It is widely used to approximate real compression/expansion in cylinders, compressors, and turbines when the path is between isothermal and adiabatic behavior.
Typical reference values are: n = 0 (constant pressure), n = 1 (isothermal ideal-gas limit), n = γ (reversible adiabatic for an ideal gas), and very large n trending toward constant volume. In practice, fitted values such as 1.2–1.4 are common for gas compression with cooling losses.
With a known n, the end state is obtained from P1·V1n = P2·V2n. If you know P2, the calculator solves V2; if you know V2, it solves P2. The tool also reports converted SI values to keep unit consistency.
For a fixed amount of ideal gas, T ∝ P·V, so temperature changes along the polytrope can be computed after P2 and V2 are determined. When T2 is the known target and n ≠ 1, the calculator uses T·Vn−1 = const to solve the final volume and then pressure.
The boundary work is the most common engineering output. For n ≠ 1, W = (P2·V2 − P1·V1)/(1−n). For the isothermal limit n = 1, W = P1·V1·ln(V2/V1). The sign indicates whether the system does work (expansion) or receives work (compression).
If you provide moles and γ, the calculator estimates ΔU, ΔH, and heat transfer using ideal-gas relations. With cv = R/(γ−1) and cp = γR/(γ−1), it computes ΔU = N cv(T2−T1), ΔH = N cp(T2−T1), and Q = ΔU + W.
Reliable results require physically valid inputs: positive pressures/volumes, temperatures above absolute zero, and consistent targets. The calculator warns when n approaches 1 (logarithmic work form) or when optional parameters are missing. For real gases at high pressure or near condensation, treat the results as an approximation.
Engineers often infer n from measured pressure–volume data by fitting a straight line to ln(P) versus ln(V), where the slope is −n. Once n is known, you can quickly estimate end states, work, and heat trends for performance comparisons, sizing, and sanity checks during experiments.
It is an empirical exponent describing how pressure changes with volume. It indirectly captures heat transfer and losses, placing the path between isothermal and adiabatic limits.
Use n = 1 for an ideal-gas isothermal process, where temperature is effectively constant. In real systems, strong cooling can make n close to 1.
For an ideal gas undergoing a reversible adiabatic process, the relation is P·Vγ = const. It is a special polytropic case with no heat transfer.
Yes. You may choose different units for each field. The tool converts to consistent SI units internally, then reports both computed SI and display-unit results.
If n ≠ 1, it uses T·Vn−1 = const to solve V2, then computes P2 from P·Vn = const. For n = 1, isothermal implies T2 ≈ T1.
They are only needed for energy estimates (ΔU, ΔH, and Q). If omitted, the calculator still computes end-state values and boundary work.
They can be rough at best. Near phase change or at high pressure, real-gas effects matter. Use property tables or real-gas models if accuracy is critical.
Important Note: All the Calculators listed in this site are for educational purpose only and we do not guarentee the accuracy of results. Please do consult with other sources as well.