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Direction: In a simple Brayton cycle, the pressure ratio is 8 and temperature at the entrance of compressor and turbine are 300 K and 1400 K, respectively. Both compressor and gas turbine have isentropic efficiencies equal to 80%. For the gas, assume a constant value of cp (specific heat at constant pressure) equal to 1 kJ/kgK and ratio of specific heats as 1.4. Neglect changes in kinetic and potential energies.

  1. The thermal efficiency of the cycle in percentage (%) is
    1. 24.8
    2. 38.6
    3. 44.8
    4. 53.1
Correct Option: A

T4 =
T3
= 772.9K
8.2857

ηT =
T3 - T4'
⇒ 0.8 =
1400 - T4'
T3 - T41400 - 772.9

ηcycle =
(WT)actual - (WC)actual
Qs

=
(T3 - T4') - (T2' - T1)
T3 - T2'

ηcycle=
(1400 - 898.32) - (604.3 - 300)
1400 - 604.3

= .248 or 24.8%



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