Analyze Brayton cycle performance using practical operating inputs. See shaft, net, and electrical output clearly. Create dependable results for design reviews and feasibility studies.
Use consistent values for compressor, turbine, fuel, and losses. The calculator applies a simplified Brayton cycle with constant specific heat.
Use this sample set to test the calculator and compare your own values.
| Parameter | Sample Value | Unit |
|---|---|---|
| Air Mass Flow | 25 | kg/s |
| Inlet Pressure | 101.325 | kPa |
| Inlet Temperature | 15 | °C |
| Pressure Ratio | 10 | ratio |
| Compressor Efficiency | 82 | % |
| Turbine Inlet Temperature | 1100 | °C |
| Turbine Efficiency | 87 | % |
| Combustor Pressure Loss | 4 | % |
| Mechanical Efficiency | 98 | % |
| Generator Efficiency | 96 | % |
| Specific Heat Cp | 1.005 | kJ/kg·K |
| Gamma | 1.4 | ratio |
| Fuel LHV | 43 | MJ/kg |
| Combustion Efficiency | 99 | % |
1. Compressor ideal outlet temperature:
T2s = T1 × rp(γ - 1) / γ
2. Compressor actual outlet temperature:
T2 = T1 + (T2s - T1) / ηc
3. Turbine ideal outlet temperature:
T4s = T3 × (P4 / P3)(γ - 1) / γ
4. Turbine actual outlet temperature:
T4 = T3 - ηt × (T3 - T4s)
5. Specific compressor work:
wc = Cp × (T2 - T1)
6. Specific turbine work:
wt = Cp × (T3 - T4)
7. Specific heat added:
qin = Cp × (T3 - T2)
8. Fuel-air ratio:
f = qin / (ηcomb × LHV)
9. Net cycle power:
Pnet = (ṁgas × wt) - (ṁair × wc)
10. Shaft and electrical power:
Pshaft = Pnet × ηm
Pelectric = Pshaft × ηg
It estimates gas turbine electrical output, shaft power, fuel use, turbine work, compressor work, net cycle power, efficiency, and key temperatures using Brayton cycle assumptions.
Pressure ratio strongly affects compressor work and turbine expansion. A better ratio can improve net output, but very high values may also raise compressor losses.
No. It is best for screening, comparison, and preliminary studies. Detailed guarantees need manufacturer maps, cooling flows, humidity effects, and part-load corrections.
Constant values simplify the Brayton cycle math. Real gas properties vary with temperature and composition, so this method trades some precision for speed and clarity.
Higher turbine inlet temperature usually increases turbine work and net power. It can also improve efficiency, provided material limits and cooling needs remain acceptable.
Pressure drops in the combustor reduce turbine expansion potential. That lowers turbine work and, in turn, reduces net cycle output and efficiency.
Specific fuel consumption shows how much fuel is needed for each kilowatt-hour of electricity. Lower values generally indicate better operating performance.
No. You can use other fuels too, as long as you enter a suitable lower heating value and combustion efficiency for that fuel.
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.