Air-standard ideal cycles. These model the working fluid as an ideal gas with no friction, heat loss or real combustion chemistry — real engines fall well short of these numbers.
Engineering · thermodynamics

PV Diagram

Pressure vs. volume for the classic ideal engine cycles.
state-by-state ideal gas law
Otto · r=8

Cycle

Parameters

Cycle diagram

Otto air-standard, ideal gas
Cycle performance
State points
StateP (kPa)V (L)T (K)
Field notes

Reading a PV diagram

How it works

The area inside the loop is the work

Every point on a PV diagram is a state of the gas — a pressure and volume (and, via the ideal gas law, a temperature). Move along a curve and the gas does work, W = ∫P dV — literally the area under that segment. A full cycle traces a closed loop, and the net work output is the area enclosed by the loop: clockwise means net work is done by the gas — an engine. This tool solves every state point exactly from the ideal gas law and each process's own equation (isochoric, isobaric, isothermal, or adiabatic), then integrates for work and heat directly — nothing here is a canned efficiency number, it's computed state by state and cross-checked against the standard closed-form efficiency formula for each cycle.

Worked example

An Otto cycle (petrol engine) at a compression ratio of 8:1 — typical for a road-car engine — has an ideal air-standard efficiency of 56.5%, from the closed form η = 1 − r^(1−γ). Real engines manage roughly half that once friction, heat loss and real combustion are accounted for — the ideal cycle is a ceiling, not a prediction.

Why is Diesel more efficient than Otto at the same compression ratio?

Diesel engines run much higher compression ratios in practice (16–22:1 vs. roughly 8–12:1 for petrol) precisely because they inject fuel only at the top of the stroke, avoiding the pre-ignition ("knock") that limits how far a petrol/air mixture can be compressed — the higher ratio, not the cycle shape itself, is what usually gives Diesel engines their efficiency edge in practice.

Why does Carnot only depend on temperature?

Carnot's cycle is built entirely from reversible isothermal and adiabatic steps, and for those the Second Law fixes the efficiency purely by the hot and cold reservoir temperatures — it's the theoretical ceiling no real heat engine operating between those two temperatures can exceed, regardless of working fluid or mechanism.

What does the Brayton cycle actually power?

Gas turbines and jet engines — continuous-flow compression, combustion and expansion rather than a piston's stop-start strokes, which is exactly why its efficiency depends on pressure ratio instead of the volumetric compression ratio the piston cycles use.

Where does the ideal cycle break down in a real engine?

Real gases aren't ideal, combustion isn't instantaneous heat addition, compression and expansion aren't frictionless or adiabatic, and every real cycle loses heat through the cylinder walls — each of these gaps costs real efficiency the air-standard analysis can't see.