NASA STI Repository (National Aeronautics and Space Administration) · 1991 · 87 citations · 3 references
Open access
EngineeringChemical EngineeringHeat TransferThermodynamicsTransport PhenomenaChemical ThermodynamicsHeat ConductionMass TransferMixture ThermodynamicsThermodynamic VariablesTransport PropertiesCompressibilityCompressibility FactorCompressibility Factor Of AirEquilibriumGas Transport PropertiesPrandtl NumberSpecific Heat CapacityThermal Conductivity
A self-consistent set of equilibrium air values were computed for enthalpy, total specific heat at constant pressure, compressibility factor, viscosity, total thermal conductivity, and total Prandtl number from 500 to 30,000 K over a range of 10(exp -4) atm to 10(exp 2) atm. The mixture values are calculated from the transport and thermodynamic properties of the individual species provided in a recent study by the authors. The concentrations of the individual species, required in the mixture relations, are obtained from a free energy minimization calculation procedure. Present calculations are based on an 11-species air model. For pressures less than 10(exp -2) atm and temperatures of about 15,000 K and greater, the concentrations of N(++) and O(++) become important, and consequently, they are included in the calculations determining the various properties. The computed properties are curve fitted as a function of temperature at a constant value of pressure. These curve fits reproduce the computed values within 5 percent for the entire temperature range considered here at specific pressures and provide an efficient means for computing the flowfield properties of equilibrium air, provided the elemental composition remains constant at 0.24 for oxygen and 0.76 for nitrogen by mass.
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Finite difference methods of solution of the boundary-layer equations
F.G. Blottner · AIAA Journal · 1970 · 394 citations
Air transport coefficients from electric arc measurements
R. S. Devoto, Uwe Bauder, Johnny G. Cailleteau et al. · The Physics of Fluids · 1978 · 40 citations