Math 2.0

Classical thermodynamics, heat transfer Thermodynamic cycles Example

Brayton cycle

Builds on Ideal gasIsentropic processIsobaric processHeat capacity ratioHeat capacityThermal efficiencyHeat engine

Example

Take nn moles of an ideal gas with constant molar heat capacity cpc_p at constant pressure and constant heat capacity ratio γ>1\gamma > 1. Let p2>p1p_2 > p_1 be two pressures, with pressure ratio rp=p2/p1r_p = p_2/p_1. The ideal Brayton cycle has four steps, with temperatures T1,T2,T3,T4T_1, T_2, T_3, T_4 at their start points:

  1. isentropic compression from p1p_1 to p2p_2;
  2. isobaric heat addition at p2p_2, absorbing QH=ncp(T3−T2)Q_H = n c_p (T_3 - T_2);
  3. isentropic expansion from p2p_2 to p1p_1;
  4. isobaric heat rejection at p1p_1, rejecting QC=ncp(T4−T1)Q_C = n c_p (T_4 - T_1), back to the initial state.

The gas returns to its initial state, so this is a thermodynamic cycle. On an isentrope of an ideal gas Tp(1−γ)/γT p^{(1-\gamma)/\gamma} is constant, so T2/T1=T3/T4=rp(γ−1)/γT_2/T_1 = T_3/T_4 = r_p^{(\gamma-1)/\gamma}. Hence T3−T2=rp(γ−1)/γ(T4−T1)T_3 - T_2 = r_p^{(\gamma-1)/\gamma} (T_4 - T_1), and the thermal efficiency is η=1−QCQH=1−rp−(γ−1)/γ.\eta = 1 - \frac{Q_C}{Q_H} = 1 - r_p^{-(\gamma - 1)/\gamma}. For rp=10r_p = 10 and γ=1.4\gamma = 1.4, η=1−10−2/7≈0.48\eta = 1 - 10^{-2/7} \approx 0.48.

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  1. Heat capacity concept
  2. Heat capacity ratio concept
  3. Heat engine concept
  4. Ideal gas concept
  5. Isentropic process concept
  6. Isobaric process concept
  7. Thermal efficiency concept
  8. Brayton cycle example

Further reading

  1. Web https://en.wikipedia.org/wiki/Brayton_cycle
About this page
Tag9GZ4K1GA16
URIm2://9GZ4K1GA16
Kindexample
WritingW0 stub
MSC80A10, 80A05
Instance ofThermodynamic cycle
UsesIdeal gas, Isentropic process, Isobaric process, Heat capacity ratio, Heat capacity, Thermal efficiency, Heat engine
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Changed3 November 2026

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