Optimization of turbojet engine cycle with dual-purpose PSO algorithm

Open Access

Table 2

Exergy efficiency and loss, and entropy production in different components of the engine at sea level and speed of 200 m/s.

Component
Diffuser	73.1	22.85	7.66
Compressor	4.00	38.01	12
Combustion chamber	51.50	2596.03	870
Turbine	25.7	112.25	38
After burner	11.6	404.68	136
Exhaust nozzle	68.6	967.54	325

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