Tables of the Thermodynamic Properties of Air and the Exhaust Gas from a Turbine Engine
Final rept. 31 Jul 1972-30 Jun 1974
ARO INC ARNOLD AFS TN
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Thermodynamic properties of air and the exhaust gas from a turbine engine CnH1.95nAir System are presented in tabular form. The properties presented air enthalpy h, entropy s, and specific heat at constant pressure cp. The properties of air are presented for a temperature range from 300 to 1, 800R and a pressure range from 0.5 to 600 psia. The properties of exhaust gas are presented for a temperature range from 600 to 4,000R, a pressure range from 0.5 to 600 psia, and a fuel-to-air ratio from 0.005 to 0.067.
- Physical Chemistry
- Jet and Gas Turbine Engines