Thermal Efficiency Calculator

Calculate thermal efficiency for Carnot, Otto, Diesel, Brayton, and Rankine cycles. Compare actual vs ideal efficiency with energy flow visualization.

kW
kW
kW

Temperature Limits

K
K
Actual Efficiency
40.00%
W_out/Q_in = 400.0/1,000.0
Carnot Limit
50.00%
1 − 300K/600K
Generic Heat Engine Ideal
50.00%
η = W_out / Q_in
2nd Law Efficiency
80.0%
η_actual / η_Carnot
Heat Rejected
600.0 kW
Q_in − W_out = waste heat
Energy Balance
40.0% useful
60.0% rejected
Energy Flow Sankey
Q_in
1,000
W_out (40%)
Q_out (60%)
W: 400
Q: 600
CycleTypical η (%)T_hot RangeApplication
Carnot60-70AnyTheoretical maximum
Combined cycle55-631400-1600°CPower plants
Brayton (gas turbine)30-401000-1500°CJet engines, peaker plants
Rankine (steam)30-45500-600°CCoal/nuclear power
Otto (gasoline)25-352000-2500°CCars, small engines
Diesel35-451800-2300°CTrucks, ships, generators
Stirling30-40700-1000°CCHP, solar dish
Planning notes, formulas, and examples

About the Thermal Efficiency Calculator

The **Thermal Efficiency Calculator** computes the thermal efficiency of common heat-engine cycles, including Carnot, Otto, Diesel, Brayton, and Rankine. Thermal efficiency is the fraction of heat input that becomes useful work, so it is the standard way to describe how well an engine turns thermal energy into output.

The Carnot cycle provides the theoretical ceiling, and real engines always fall below it because of friction, finite heat transfer, pressure losses, and other irreversibilities. That contrast makes the page useful when you want to compare actual engine performance against the ideal limit.

Alongside first-law efficiency, the calculator can show second-law efficiency and cycle-specific reference values so you can judge whether a result is merely reasonable or unusually close to the thermodynamic limit.

When This Page Helps

Thermal efficiency is the quickest way to compare one engine or cycle against another because it reduces the heat-flow story to a single output fraction. That helps when you are checking whether a design is competitive, whether a change improved performance, or how far a real machine sits below the ideal cycle.

How to Use the Inputs

  1. Select a cycle type: Carnot, Otto, Diesel, Brayton, Rankine, or generic.
  2. Enter heat input, heat rejected, and work output.
  3. Enter hot source and cold sink temperatures for Carnot limit calculation.
  4. For Otto/Diesel, enter the compression ratio and specific heat ratio.
  5. For Brayton, enter the pressure ratio.
  6. Use presets for common engine types to see typical values.
  7. Compare actual efficiency against the Carnot and ideal cycle limits.
Formula used
η = W_out / Q_in (First law thermal efficiency) Carnot: η = 1 − T_cold/T_hot Otto: η = 1 − 1/r^(γ−1) Diesel: η = 1 − [1/r^(γ−1)] × [(rc^γ − 1)/(γ(rc − 1))] Brayton: η = 1 − 1/rp^((γ−1)/γ) Second law: η_II = η_actual / η_Carnot

Example Calculation

Result: 40% (actual), 60.2% (ideal Otto)

Actual η = 1000/2500 = 40%. Ideal Otto η = 1 − 1/10^0.4 = 60.2%. Second law efficiency with Carnot limit at these temperatures would indicate how close the engine operates to the theoretical maximum. The gap between 40% and 60.2% represents losses from incomplete combustion, heat transfer during compression/expansion, and friction.

Tips & Best Practices

  • Carnot efficiency only depends on temperatures — higher T_hot and lower T_cold give better efficiency.
  • Real engine efficiency is typically 40-70% of the Carnot limit due to irreversibilities.
  • Compression ratio is the single most important parameter for reciprocating engine efficiency.
  • Combined heat and power (CHP) captures waste heat, reaching 80-90% total energy utilization.
  • Electric motors are 90-98% efficient — incomparably better than heat engines for mechanical work.
  • Waste heat recovery (ORC, thermoelectric) can add 5-15% to overall system efficiency.

Thermodynamic Cycles in Detail

**Carnot Cycle:** The theoretical ideal consists of two isothermal and two adiabatic processes. No real engine achieves Carnot efficiency because isothermal heat transfer requires infinite time (infinitely slow processes). The Carnot cycle provides the absolute efficiency ceiling for any heat engine operating between two temperature reservoirs.

**Otto vs. Diesel:** The Otto cycle (constant-volume combustion) describes spark-ignition gasoline engines. The Diesel cycle (constant-pressure combustion) describes compression-ignition engines. At the same compression ratio, Otto efficiency exceeds Diesel due to the cutoff ratio penalty. However, Diesel engines use much higher compression ratios, giving them better real-world efficiency.

Efficiency Trends in Power Generation

Modern power generation has pushed thermal efficiency steadily upward. Coal plants evolved from 25% (1920s) to 45% (modern supercritical). Gas turbines improved from 35% simple cycle to 63% combined cycle. The thermodynamic limit for combined cycles at 1600°C turbine inlet temperature and 20°C ambient is about 70%.

Nuclear power plants operate at lower temperatures (~330°C for PWRs) due to material limitations in the reactor, resulting in relatively modest 33-37% thermal efficiency. Advanced reactor designs (molten salt, gas-cooled) aim for 45-50% by reaching higher temperatures.

Beyond Carnot: Practical Considerations

Real engines face losses that reduce efficiency below ideal cycle values: friction in bearings and piston rings, pressure drops in flow paths, incomplete combustion, heat leak through cylinder walls, pumping losses (intake/exhaust), and auxiliary power consumption. The ratio of actual to ideal efficiency (sometimes called relative efficiency or isentropic efficiency) ranges from 70-85% for well-designed engines.

Sources & Methodology

Last updated:

Frequently Asked Questions

  • The second law of thermodynamics requires that some heat must be rejected to a cold sink. Even a perfect (Carnot) engine between 600K and 300K can only achieve 50% efficiency. The remaining 50% must be rejected — this is a fundamental law of nature, not an engineering limitation.