Optimization of turbojet engine cycle with dual-purpose PSO algorithm

Open Access

Table 5

Optimal values at different altitudes.

H			M				r_c
1000	1189.9	47.7	0.6	88	80	80	7
3000	1142.8	50.06	0.6	92	80	86	7
5000	1101.2	53.23	0.99	94	94	94	9.98

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