The nominal values used for air at 300 K are CP = 1.00 kJ/kg.K, Cv = 0.717 kJ/kg.K,, and k = 1.4. However they are all functions of temperature, and with the extremely high temperature range experienced in internal combustion and gas turbine engines one can obtain significant errors. Potter & Somerton suggest that in those cases one should consult ideal gas tables in Appendix E, which tabulate h(T) and u(T), or integrate using expressions for CP(T) found in Table B-5 (however Table B-5 does not include values for air!). An alternative approach which we find gives results with reasonable accuracy (within around 1%) is to use values of specific heats at the average value of temperature T in each process. This is conveniently done using tables of specific heats vs T, however since Potter & Somerton do not provide these we have provided one here for air:
Ideal gas specific heat capacities of air Temperature
KCP
kJ/kg.KCv
kJ/kg.Kk 250 1.003 0.716 1.401 300 1.005 0.718 1.400 350 1.008 0.721 1.398 400 1.013 0.726 1.395 450 1.020 0.733 1.391 500 1.029 0.742 1.387 550 1.040 0.753 1.381 600 1.051 0.764 1.376 650 1.063 0.776 1.370 700 1.075 0.788 1.364 750 1.087 0.800 1.359 800 1.099 0.812 1.354 900 1.121 0.834 1.344 1000 1.142 0.855 1.336 1100 1.155 0.868 1.331 1200 1.173 0.886 1.324 1300 1.190 0.903 1.318 1400 1.204 0.917 1.313 1500 1.216 0.929 1.309
The values up to 1000 K were originally published in "Tables of Thermal Properties of Gases", NBS Circular 564,1955. The last five rows were calculated from a formula by B G Kyle "Chemical and Process Thermodynamics", Englewood Cliffs / Prentice Hall, 1984, and have <1% error.