Title of article :
A High-Temperature, Thermal Non-equilibrium Equation of State for Ammonia
Author/Authors :
D. L. Allison and P. G. Mikellides ، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2006
Pages :
26
From page :
794
To page :
819
Abstract :
The engineering applications of ammonia extend far beyond the pressure and temperature ranges for which thermodynamic models currently exist in the literature. Thus, a thermal non-equilibrium thermochemical model was developed to compute the composition and thermodynamic properties of ammonia for an extended temperature and pressure range that includes ionization reactions. Thermal non-equilibrium between electrons and heavy particles was included and is preseInted for ratios of 1/2, 1, 2, and 3. The fourteenequation nonlinear system produced under the assumptions of ideal gas and two-temperature local thermodynamic equilibrium was solved numerically using a Newton-Raphson method. The thermochemical model is verified for both the composition and thermodynamic properties by comparisons to existing thermochemical models in the literature. These comparisons verify the model for the available, yet limited, temperature and density ranges. Analysis of the composition and thermodynamic properties as a function of the independent properties confirms the necessity for such a model as part of rigorous computations with computational fluid dynamics (CFD) or magnetohydrodynamics (MHD) computer codes. The model can be easily cast in tabular form to complement the set of conservation equations utilized by such codes.
Keywords :
Ammonia , Equation of state , electric rocket propellant , hightemperaturethermochemical model , Thermal non-equilibrium
Journal title :
International Journal of Thermophysics
Serial Year :
2006
Journal title :
International Journal of Thermophysics
Record number :
427354
Link To Document :
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