Brayton ·
Cycle
un
seel
.com · gas turbine · jet engine · η = 1 − r_p^((1−γ)/γ)
Pressure ratio r_p
30
η_ideal
62.1%
phase
—
1 inlet (cold)
2 after compressor
3 after combustor (hot)
4 after turbine (exhaust)
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.com · Brayton Cycle