Two engines. One clever idea.

Follow the exhaust. See how hot gas powers a turbine in both engines.

Exhaust turns the turbine. The shaft carries the power.

Both use hot gas to turn a turbine, then a shaft to power a compressor. Follow the orange gas through each highlighted turbine and the green shaft back to the compressor.

Jet engine

Continuous combustion

Combustor → turbine → nozzle

Turbine power, then nozzle thrust.

Hot gas gives up some energy to drive the compressor through the turbine shaft. Gas leaving the turbine still has energy to accelerate through the nozzle.

Idle45%High
Thrust response
Fresh airHot gasShaft power
Click a labeled part to explore it.

Explore a component

The compressor

Rotating blades squeeze incoming air. The turbine supplies the power through a shared shaft.

Higher-pressure air enters the combustor, where fuel is added and burned.

In both engines, hot gas turns a turbine. Its shaft transfers that energy to a compressor.

Sources & model notes

How to read the demo

These are simplified teaching cutaways, shown in slow motion. Dots trace gas paths; their spacing and speed are not measurements of pressure, temperature, or flow. Green shafts show mechanical power, not gas passages.

Power demand changes an illustrative operating state. Both rotors respond gradually. Car boost lags a change in demand because the turbo needs time to speed up. The response bars are normalized within each engine; they are not comparable performance measurements. Their time constants are animation choices.

Slow motion changes playback speed only. Pause freezes both the mechanism and its response. Selecting a stroke pauses at that stroke's midpoint. The car is a four-stroke petrol engine: intake, compression, power, exhaust over two crankshaft revolutions (720°). The simplified valve timing omits overlap; a real engine's timing and ignition vary.

The turbo and crankshaft rotate independently. The intercooler removes heat from compressed intake air. In the jet, combustion stays continuous and all stages operate together. The optional turbofan view schematically shows a separate fan turbine and shaft; blade counts and geometry are illustrative.

Learn more

  1. NASA · Turbojet thrustCompressor, combustor, turbine, shaft, and nozzle.
  2. NASA · Turbofan thrustCore flow, bypass flow, and the fan's turbine drive.
  3. NASA · The four-stroke enginePistons, crankshaft, and the repeated combustion cycle.
  4. Garrett · How a turbo worksThe separate intake and exhaust sides, and charge-air cooling.
  5. Garrett · Turbocharging factsExhaust-driven compression and turbo lag.

Original interactive illustrations. No measured engine data or performance prediction.