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Thermal Efficiency of a Heat Engine

Thermal efficiency measures how much of the heat added to an engine is converted into useful work. It equals net work output divided by heat input. For example, a car engine might have a thermal efficiency of 30%, meaning 70% of the fuel's energy is lost as heat in the exhaust and cooling system. It is always less than the Carnot efficiency. Improving it is a major goal in engine design.

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Thermal Efficiency Calculator — Heat Engine

Solve the classic heat-engine efficiency relation η = Wnet / Qin for any of its three quantities — thermal efficiency, net work output, or heat input — with step-by-step math, a live energy-flow Sankey diagram, an efficiency gauge, and companion metrics including Carnot comparison and heat rate.

η = Wnet / Qin · Qin = Wnet + Qout
Solve for
Engine presets
Thermal Efficiency (η) Ratio of net work output to heat input, expressed as a percentage. The second law of thermodynamics caps η at the Carnot efficiency 1 − TC/TH, so no real heat engine can reach 100%. Typical values: 25–30% for spark-ignition engines, 35–42% for diesels and industrial gas turbines, 55–62% for combined-cycle plants.
%
Efficiency must be between 0 and 100%.
Net Work Output (Wnet) Useful work delivered by the engine per cycle, in kilojoules (or kilowatts if you are working with rates — the ratio is dimensionless either way). Net work is the gross work produced by expansion minus the work consumed by compression and auxiliary systems. It equals Qin − Qout by the first law.
kJ
Net work cannot be negative or exceed the heat input.
Heat Input (Qin) Thermal energy supplied to the working fluid from the hot reservoir, per cycle. In a combustion engine it is the fuel's chemical energy released by burning; in an external-combustion engine it is heat transferred from a hot source. Must be greater than zero. Qin = Wnet + Qout by the first law.
kJ
Heat input must be greater than zero.
Hot Reservoir Temperature (TH) — optional Absolute temperature of the hot reservoir, in kelvin. Used only for the Carnot comparison: the second law caps efficiency at ηCarnot = 1 − TC/TH. To convert from °C, add 273.15. Typical: 500–800 K for an engine block, 1200–1800 K for combustion gases, 550–900 K for a steam turbine's superheated inlet.
K
Cold Reservoir Temperature (TC) — optional Absolute temperature of the cold reservoir (typically the environment), in kelvin. The Carnot limit ηCarnot = 1 − TC/TH improves as TC falls, which is why power plants use cooling towers or river water. Ambient air is about 300 K; cooling water can be 290 K or lower.
K
THERMAL EFFICIENCY (η)
40.00 %
η = 0.4000 · Qout = 600 kJ · 62.5% of Carnot
GOOD — 35–45% (DIESEL / INDUSTRIAL TURBINE)
η = W_net / Q_in
Step-by-step solution
η vs. net work Wnet (three heat inputs)
Current Qin Qin × 0.7 Qin × 1.4
η vs. heat input Qin (three work outputs)
Current Wnet Wnet × 0.7 Wnet × 1.4
Energy split — Wnet vs. Qout
Useful work Wnet Rejected heat Qout
Sensitivity
Companion thermodynamics metrics
Energy flow through the heat engine — live Sankey
ENERGY CONSERVATION · Q_in = W_net + Q_out · η = W_net / Q_in HEAT ENGINE η = 40.0% Wout − Win = Wnet Qin 1000 kJ Wnet 400 kJ Qout 600 kJ Arrow thickness ∝ energy · first law holds exactly EFFICIENCY GAUGE 40.0% thermal efficiency 0% 100% LIVE VALUES — — — — — —
Heat input Qin Net work output Wnet Rejected heat Qout Carnot efficiency limit (if TH, TC given)
What the thermal efficiency relation really measures
ηthermal efficiency
=
Wnetnet work out
/
Qinheat in

Efficiency is a first-law ratio

The definition η = Wnet/Qin is purely an energy accounting statement: of all the heat you put in, what fraction came out as useful work? The rest is rejected as Qout. This is the first law of thermodynamics applied to a cyclic device — energy in equals energy out. It says nothing about whether the process is reversible or what the maximum achievable efficiency is; that question belongs to the second law.

The second law caps efficiency below 100%

No heat engine can convert all of its heat input into work. The Carnot limit ηCarnot = 1 − TC/TH is the absolute maximum for any engine operating between reservoirs at those absolute temperatures, and it is achieved only by a fully reversible cycle (infinitely slow, no friction, no heat leaks). Real engines reach 50–80% of Carnot, with the shortfall coming from finite-rate heat transfer, friction, turbulence, and combustion irreversibility.

Raising TH helps more than lowering TC

The Carnot formula is more sensitive to TH than to TC in the typical operating range. Starting from TH = 800 K and TC = 300 K, raising TH by 100 K improves ηCarnot from 62.5% to 66.7%, while lowering TC by 100 K only improves it to 70.0% — but reaching TC = 200 K requires refrigeration, whereas raising TH only requires better materials. This is why gas turbines with turbine inlet temperatures above 1700 K dominate the efficiency race, and why metallurgy and blade cooling are such active research areas.

Efficiency, heat rate, and fuel cost are linked

The heat rate HR = 3600/η (in kJ per kWh) is the fuel energy required per unit of electrical or mechanical output. At η = 40%, HR = 9000 kJ/kWh, which is about 8532 BTU/kWh — a familiar figure in power plant engineering. A one-point improvement in efficiency (say 40% → 41%) reduces heat rate by about 220 kJ/kWh, and on a 500 MW plant running 8000 hours a year that saves roughly 880 TJ of fuel, worth millions of dollars. This is why utilities pursue single-percentage-point efficiency gains so aggressively.

How to Use This Calculator

The thermal efficiency relation links three quantities: η, Wnet, and Qin. Pick which one you want the tool to solve, then fill in the other two.

1. Choose what to solve for

Pick η, Wnet, or Qin from the toggle. The calculator rearranges η = Wnet/Qin for whichever variable you choose, and always derives Qout = Qin − Wnet as a companion metric.

2. Start from an engine preset

Presets cover the practical range: an ideal Carnot cycle at 62.5%, a gasoline SI engine at 28%, a diesel at 38%, an industrial gas turbine at 40%, a steam turbine at 38%, a combined cycle at 58%, and a Stirling engine at 35%. Each preset sets realistic Qin, Wnet, TH, and TC.

3. Add reservoir temperatures for Carnot comparison

Entering TH and TC in kelvin unlocks the second-law comparison: the Carnot efficiency limit, the fraction of Carnot your engine achieves, and the theoretical headroom available for improvement. If you only have °C, add 273.15 to convert.

4. Watch the first-law constraint

Net work can never exceed heat input — that would violate the first law and give η > 100%. The calculator flags this case. It also flags negative work, which would mean the engine is acting as a heat pump or refrigerator rather than a heat engine.

5. Read the result, diagram, and gauge

The result card shows the solved value with the energy split and the fraction of Carnot. The Sankey diagram shows Qin splitting into Wnet and Qout with arrow thicknesses proportional to energy. The semicircular gauge shows η on a 0–100% scale, with a dashed marker for the Carnot limit when temperatures are given.

6. Switch to Advanced for depth

Advanced mode adds a chart of η vs. Qin, a stacked bar chart of the Wnet/Qout energy split, a sensitivity panel, and companion thermodynamics metrics including heat rate in kJ/kWh and BTU/kWh, the fraction of Carnot, and the theoretical maximum work.

What This Tool Offers

Built around the classic heat-engine efficiency relation η = Wnet / Qin, the fundamental link between heat input, useful work, and rejected heat.

Three-way solving

Solve for efficiency, net work output, or heat input. The calculator rearranges the relation for whichever variable you choose and always derives the rejected heat Qout.

Live energy Sankey

A Sankey diagram with arrow thickness proportional to energy, showing Qin splitting into Wnet and Qout through the engine. First-law conservation is visible at a glance.

Efficiency gauge

A semicircular gauge plots η on a 0–100% scale, with a dashed marker for the Carnot limit whenever TH and TC are entered — so the second-law headroom is always visible.

Carnot comparison

Enter hot and cold reservoir temperatures to compute the Carnot efficiency limit, the fraction of Carnot your engine achieves, and the theoretical maximum work available.

Three comparison charts

η vs. Wnet for three heat inputs, η vs. Qin for three work outputs, and a stacked bar chart of the Wnet / Qout split.

Reference tables

Typical efficiency by engine type, an efficiency lookup grid across several heat inputs, a unit converter between kJ, kWh, and BTU, and a full variable reference table.

Reference Tables & Conversions

An energy converter, an efficiency lookup grid, and typical values by engine type.

Energy unit converter

kJ
kWh
BTU
kcal
%
kJ/kWh
= 1,000 kJ = 0.27778 kWh = 947.82 BTU = 239.01 kcal · η 40% → HR 9000 kJ/kWh

Efficiency Lookup — η = Wnet / Qin

Computed for the net work values shown across several heat inputs. Values in percent.

Wnet (kJ)Qin = 200Qin = 500Qin = 1000Qin = 2000Qin = 5000Qin = 10000

Typical Thermal Efficiency by Engine Type

Representative real-world values at rated conditions. Efficiency varies strongly with load, ambient temperature, and maintenance.

Engine typeTypical ηTypical THTypical TCFraction of CarnotNotes
Carnot (theoretical)ηCarnot——100%Reversible ideal, unattainable in practice
Stirling (external combustion)30–40%~1000 K~300 K~50%High theoretical efficiency, low power density
Spark-ignition gasoline25–30%~2200 K flame, ~800 K metal~350 K~45%Throttling and knock limit compression ratio
Compression-ignition diesel35–42%~2200 K flame, ~900 K metal~350 K~55%Higher compression ratio, no throttling
Industrial gas turbine (simple)35–42%~1600 K~300 K~55%Turbine inlet temperature is the limiting factor
Steam turbine (coal)33–40%~800 K~300 K~60%Supercritical steam reaches the upper end
Combined cycle (gas + steam)55–62%~1600 K~300 K~75%Best commercial efficiency today
Nuclear steam cycle32–37%~600 K~300 K~60%Lower TH to stay within cladding limits
Fuel cell (hydrogen)45–60%~350 K~300 K—Not a heat engine; not bound by Carnot

Variable Reference

SymbolMeaningTypical rangeUnits
ηThermal efficiency0.05 – 0.62— (or %)
WnetNet work output per cycle0 – 10⁶kJ (or kW)
QinHeat input per cycle0 – 10⁶kJ (or kW)
QoutRejected heat per cycle0 – 10⁶kJ (or kW)
THHot reservoir temperature300 – 2000K
TCCold reservoir temperature250 – 400K
ηCarnotCarnot efficiency limit0 – 1—
HRHeat rate = 3600 / η5800 – 20000kJ/kWh

What Does η = Wnet / Qin Measure?

The thermal efficiency of a heat engine is the fraction of the heat supplied to it that emerges as useful work. It answers a direct and practical question: for every unit of fuel energy burned, how much mechanical or electrical output do I get? The relation η = Wnet/Qin is the definition, and it follows from the first law of thermodynamics applied to a cyclic device — energy in equals energy out, so whatever is not converted to work must be rejected as heat.

This definition is universal: it applies to a car engine, a power station steam turbine, a jet engine, a Stirling engine, and a fuel cell. What differs between them is the achievable value of η. The second law of thermodynamics sets the ceiling — the Carnot efficiency 1 − TC/TH — and real engines fall short of that ceiling by an amount that depends on how irreversible their internal processes are. Understanding both the definition and the limit is essential for anyone sizing, selecting, or improving an energy conversion system.

Thermal Efficiency Formula

The defining relationship is:

η = Wnet / Qin

Rearranged to solve for the other two quantities:

Wnet = η · Qin
Qin = Wnet / η

Companion relations that follow directly from the first and second laws:

Energy balance: Qin = Wnet + Qout
Alternative form: η = 1 − Qout / Qin
Carnot limit: ηCarnot = 1 − TC / TH   (T in kelvin)
Fraction of Carnot: fC = η / ηCarnot
Heat rate: HR = 3600 / η   (kJ per kWh)
Maximum work (Carnot): Wmax = ηCarnot · Qin

For an engine operating at power rather than per cycle, the same relations apply with Qin replaced by the heat input rate Q̇in (in kW) and Wnet by the net power output Pnet (in kW). The ratio is unchanged.

Thermal Efficiency Variables

SymbolMeaningNotes
ηThermal efficiencyDimensionless; often expressed as a percentage
WnetNet work outputGross expansion work minus compression and auxiliary work
QinHeat inputThermal energy supplied from the hot reservoir per cycle
QoutRejected heatEnergy dumped to the cold reservoir; Qout = Qin − Wnet
THHot reservoir temperatureAbsolute temperature in kelvin
TCCold reservoir temperatureUsually the ambient or cooling-water temperature
ηCarnotCarnot efficiency limitTheoretical maximum for the given reservoirs
HRHeat rateFuel energy per unit of output; lower is better

How Each Variable Affects the Efficiency

The relation is linear in Wnet and inversely proportional to Qin. Halving the heat input for the same work doubles the efficiency; doubling the work for the same heat input also doubles the efficiency. In practice, engine designers attack both sides at once: they increase Wnet by improving combustion, reducing friction, and recovering exhaust energy, while reducing Qin per unit of output by raising the compression ratio, using higher-energy fuels, or improving combustion phasing.

The Carnot limit provides the context. If TH = 800 K and TC = 300 K, the ceiling is 62.5%. An engine achieving 40% is therefore capturing 64% of the available theoretical work — an impressive figure for a real machine. Improving that to 45% requires either raising TH, lowering TC, or reducing irreversibility. Raising TH is usually the most accessible lever, but it is limited by the materials that can survive the higher temperatures without melting, creeping, or oxidizing. That is why the history of engine efficiency is largely the history of high-temperature materials: nickel superalloys for turbine blades, ceramic thermal barrier coatings, and single-crystal casting have all been developed specifically to allow higher TH.

Lowering TC is generally harder and more expensive. In a power plant, TC is set by the cooling medium — river water in the range 285–295 K, or ambient air at 300 K or above. Cooling towers can bring the water temperature close to the wet-bulb temperature, but they cost capital and consume water. This is why plants in cold climates achieve slightly higher efficiency than the same design in the tropics, and why a plant's efficiency is quoted at a specified reference cooling condition.

Thermal Efficiency Calculation Examples

Given: Qin = 1000 kJ, Wnet = 400 kJ — solve for η
η = 400 / 1000 = 0.40 = 40.0%
Qout = 1000 − 400 = 600 kJ
Given: η = 40%, Qin = 1000 kJ — solve for Wnet
Wnet = 0.40 × 1000 = 400 kJ
Given: η = 40%, Wnet = 400 kJ — solve for Qin
Qin = 400 / 0.40 = 1000 kJ
Given: TH = 800 K, TC = 300 K — solve for the Carnot limit
ηCarnot = 1 − 300/800 = 1 − 0.375 = 0.625 = 62.5%
Given: η = 40%, ηCarnot = 62.5% — solve for the fraction of Carnot
fC = 0.40 / 0.625 = 0.64 = 64%
Given: η = 40% — solve for the heat rate
HR = 3600 / 0.40 = 9000 kJ/kWh = 8532 BTU/kWh
Given: Qin = 1000 kJ, Wnet = 400 kJ, TH = 800 K, TC = 300 K — solve for the available headroom
Wmax = ηCarnot · Qin = 0.625 × 1000 = 625 kJ
Headroom = 625 − 400 = 225 kJ additional work theoretically available

Frequently Asked Questions

Because the second law of thermodynamics forbids it. A heat engine works by taking heat from a hot reservoir, converting some of it into work, and rejecting the rest to a cold reservoir. The Carnot relation ηCarnot = 1 − TC/TH gives the maximum possible efficiency for any engine operating between those two temperatures, and it is less than 1 for any finite TH and any TC above absolute zero. To achieve 100% you would need either TH = ∞ or TC = 0 K, neither of which is achievable. In physical terms, the heat rejection is not a design flaw — it is a fundamental consequence of the fact that heat flows from hot to cold and that a cyclic engine must return to its starting state.

First-law efficiency is the definition η = Wnet/Qin, sometimes called thermal efficiency or energy efficiency. It is purely an energy accounting ratio: how much of the heat you put in came out as work? Second-law efficiency — sometimes called exergy efficiency or effectiveness — compares the actual efficiency to the Carnot limit: ηII = η / ηCarnot. First-law efficiency tells you how well the engine converts fuel to work. Second-law efficiency tells you how close the engine is to the thermodynamic ideal for its operating temperatures, and therefore how much room for improvement remains. A 40% efficient engine at 800 K / 300 K has a second-law efficiency of 64%, meaning there is 36% of the ideal still theoretically available.

Three main reasons. First, diesels run at higher compression ratios — typically 14–23:1 versus 8–12:1 for gasoline — which raises the effective expansion ratio and extracts more work from the hot gases. Second, diesels are unthrottled: gasoline engines throttle the intake air to control power, which costs pumping work, while diesels control power by varying the fuel injected into a full air charge. Third, diesels run lean overall, which reduces the specific heat ratio penalty. The result is a typical diesel efficiency of 35–42% versus 25–30% for a comparable gasoline engine. The trade-offs are higher NOx and particulate emissions, higher weight, and higher initial cost.

Heat rate is the reciprocal of efficiency, expressed as fuel energy per unit of useful output: HR = 3600/η in kJ/kWh, or HR = 3412/η in BTU/kWh. It is the quantity that matters for fuel cost, because it directly tells you how much fuel you burn per kilowatt-hour generated. A plant with η = 40% has HR = 9000 kJ/kWh, while a plant with η = 45% has HR = 8000 kJ/kWh — an 11% reduction in fuel consumption for the same output. Utilities track heat rate obsessively because fuel is by far the largest operating cost of a thermal power plant, typically 60–80% of the total. A one-point improvement in efficiency on a 500 MW plant saves millions of dollars per year.

By using two engines in series. A gas turbine burns fuel at very high temperature (TH around 1600 K) and produces work, but its exhaust is still hot — around 850 K. Instead of rejecting that heat to the environment, the plant routes the exhaust through a heat-recovery steam generator, which raises steam that drives a steam turbine. The steam turbine then converts additional work from heat that would otherwise have been wasted. The combined efficiency is roughly the sum of the two cycles minus overlap: 40% from the gas turbine plus 20% from the steam bottoming cycle gives about 58–62% overall. This is why combined-cycle plants dominate new natural gas power generation — they are the most efficient heat engines ever built at scale.

For a given engine cycle and given reservoir temperatures, the theoretical efficiency does not depend on the fuel — it depends only on TH and TC. In practice, however, different fuels have different combustion temperatures, flame speeds, and energy densities, which affect the achievable TH and the losses. Natural gas burns hotter and cleaner than coal, allowing higher turbine inlet temperatures in a gas turbine. Hydrogen burns hotter still, with no carbon emissions, but its storage and handling are more difficult. The fuel's energy content (higher heating value versus lower heating value) also affects the quoted efficiency, since HHV efficiency is always lower than LHV efficiency for the same engine — a fact that matters when comparing engines from different manufacturers who may use different conventions.

No, for a heat engine operating in a cycle between two thermal reservoirs, efficiency cannot exceed the Carnot limit. If you calculate an efficiency higher than Carnot, either the reservoir temperatures you entered are wrong, or the device is not a heat engine — for example, a fuel cell converts chemical energy directly to electricity without going through a heat cycle, so it is not bound by the Carnot limit. Similarly, a heat pump or refrigerator has a coefficient of performance that can be greater than 1, because it uses work to move heat rather than converting heat into work. The Carnot limit applies specifically to devices that take heat in and produce work out.

Any consistent energy or power units work, because η is a ratio. If you are analysing a single cycle, use kJ for both Wnet and Qin — that is the convention this calculator uses. If you are analysing a continuous engine running at steady state, use kW for both the net power output and the heat input rate. Other valid pairs include BTU and BTU/h, kcal and kcal/h, or MJ and MJ/s (which is the same as kW). The only rule is that both quantities must be in the same unit. Mixing units — for example kJ for work and kW for heat — is the most common source of confusion in hand calculations.

Calculating...

Variables

Symbol Quantity Unit
eta Thermal efficiency (dimensionless)
W_net Net work output of the engine kJ
Q_in Total heat input to the engine kJ

What it means

The thermal efficiency of a heat engine is a measure of its performance, defined as the ratio of the net work output to the heat supplied from the high‑temperature reservoir: η = W_net / Q_in. By the first law, W_net = Q_in − Q_out, so η = 1 − (Q_out / Q_in). This shows that to maximise efficiency, heat rejection should be minimised. The second law imposes the maximum possible efficiency (Carnot). Real engines have lower efficiencies due to irreversibilities. Thermal efficiency is a key parameter in internal combustion engines, steam turbines, and gas turbines. It affects fuel economy and emissions. Improving thermal efficiency is a major goal in engine research, through higher compression ratios, better combustion, and waste heat recovery. The efficiency of power plants is often quoted as a percentage; for example, modern combined‑cycle plants achieve around 60%. Understanding thermal efficiency is essential for energy engineering and environmental policy.

Worked example

Thermal Efficiency – Two Examples

Real‑World
Scenario 1 – Steam Engine: Net work output 100 kJ, heat input 300 kJ. Find η.
ParameterValue
W_net100 kJ
Q_in300 kJ
1η = W_net / Q_in = 100/300 ≈ 0.333 = 33.3%
Resultη ≈ 33.3%✓
Scenario 2 – Gas Turbine: Work output 250 kJ, heat input 1000 kJ. Find η.
ParameterValue
W_net250 kJ
Q_in1000 kJ
1η = 250/1000 = 0.25 = 25%
Resultη = 25%✓
Key insight: Thermal efficiency measures how effectively heat is converted to work – always less than 100%.

Common mistakes

  • Net work Wnet: It is Qin − Qout, not just the work output from a single process.
  • Heat input Qin: The heat added to the working fluid from the hot reservoir.
  • Units: Both W and Q in Joules (or kJ).
  • Efficiency < 1: Second law ensures η < 1 for any real engine.
  • Carnot comparison: The thermal efficiency is always less than or equal to the Carnot efficiency.

Applications

Thermal efficiency of a heat engine is the ratio of net work output to heat input from the hot reservoir. It indicates how effectively a heat engine converts thermal energy into mechanical work. This parameter is used to compare different engine types (e.g., Otto, Diesel, gas turbines) and to assess the performance of power plants. Improving thermal efficiency leads to lower fuel consumption and reduced emissions. Engineers apply this formula in the design of combustion chambers, heat exchangers, and cycle configurations. It also guides the selection of operating pressures and temperatures. By optimising thermal efficiency, engineers can produce more power with less environmental impact.

  • Design and optimisation of internal combustion engines
  • Gas turbine and jet engine performance assessment
  • Steam power plant cycle analysis
  • Comparison of thermodynamic cycles
  • Energy conversion system feasibility studies

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  • Published July 12, 2026
  • Last updated September 9, 2026