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Prediction of thermophysical properties of gas turbine combustion gases using the Mansour-Najjar equation of state

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  • Mansour, Awad R.

Abstract

A number of thermophysical properties of combustion gases occurring in turbine engines have been compared with experimental data by using the Mansour-Najjar equation of state. The values obtained are shown to be more accurate than those derived from the virial equation of state. The following properties were studied: density, specific heat, enthalpy, entropy, viscosity, and thermal conductivity in the temperature range 200–2600 K at pressures of 3–12 atm.

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  • Mansour, Awad R., 1988. "Prediction of thermophysical properties of gas turbine combustion gases using the Mansour-Najjar equation of state," Energy, Elsevier, vol. 13(9), pages 691-696.
    • Handle: RePEc:eee:energy:v:13:y:1988:i:9:p:691-696
    DOI: 10.1016/0360-5442(88)90101-6
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