Analyze an ideal Brayton cycle for gas-turbine concept checks and thermal efficiency studies.
Thermal efficiency
48.21%
ideal cycle
Net specific work
408.46 kJ/kg
turbine minus compressor
Back-work ratio
0.397
compressor / turbine work
Compression raises pressure and temperature, heat addition sets turbine inlet temperature, and expansion leaves net shaft work.
eta 48.2%
Heat added
847.3 kJ/kg
844 K combustor rise
Work split
408.5 kJ/kg net
back-work ratio 0.397
Pressure ratio
10.0:1
T2 556 K, T4 725 K
This tool is open source and the underlying logic is fully transparent. You can inspect the code, understand the calculations, and contribute improvements. If you want to use the tool in your own website, course page, or learning platform, you can also embed it directly and start from a ready-made iframe setup for this exact tool.
Open source: review the implementation and see how the results are produced.
Embeddable: preview this tool, copy the iframe, and use it in your own site or LMS.
Analyze an ideal Brayton cycle for gas-turbine concept checks and thermal efficiency studies.
Thermal efficiency
48.21%
ideal cycle
Net specific work
408.46 kJ/kg
turbine minus compressor
Back-work ratio
0.397
compressor / turbine work
Compression raises pressure and temperature, heat addition sets turbine inlet temperature, and expansion leaves net shaft work.
eta 48.2%
Heat added
847.3 kJ/kg
844 K combustor rise
Work split
408.5 kJ/kg net
back-work ratio 0.397
Pressure ratio
10.0:1
T2 556 K, T4 725 K
This tool is open source and the underlying logic is fully transparent. You can inspect the code, understand the calculations, and contribute improvements. If you want to use the tool in your own website, course page, or learning platform, you can also embed it directly and start from a ready-made iframe setup for this exact tool.
Open source: review the implementation and see how the results are produced.
Embeddable: preview this tool, copy the iframe, and use it in your own site or LMS.