A New Formulation of the Multicomponent Transport Equations for Use in Laminar Boundary Layer Problems
Numerically calculable transport equations derived using modified Chapman-Enskog method for laminar boundary layer problems
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Numerically calculable transport equations derived using modified Chapman-Enskog method for laminar boundary layer problems
Chapman-Enskog method modified for formulation of multicomponent laminar boundary layer problem for numerical solution
Transport coefficients for almost Lorentzian mixture, computed as perturbation to coefficients for true Lorentzian mixture, compared to Chapman-Enskog method results
The Boltzmann-Fokker-Planck equation is solved with the Chapman-Enskog method of analysis for the velocity distribution functions of helium, carbon, nitrogen, and oxygen. The analysis is a perturbation scheme based on the assumption of a collision-dominated gas, and the calculations are carried out to first order. The elements considered are treated as trace constituents in an electron-proton gas. From the resulting distribution functions, diffusion coefficients are computed which are found to be 20-30% less than those obtained by Chapman and Burgers. In addition, it is shown that the return current of cold electrons needed to maintain quasi-neutrality in a plasma with a temperature gradient contributes a term in the thermal diffusion coefficient omitted erroneously in previous works. This added term resolves the longstanding controversy over the discrepancy between the coefficients of Chapman and Burgers, which are seen to be completely equivalent in the light of this analysis. The viscosity coefficient for an electron-proton gas is also computed and found to be 7% less than that obtained by Braginskii.
Equations have been obtained for jump (or slip) in the wall values of species concentration, pressure, velocity, and temperature for the low-Reynolds-number high-altitude flight regime of a space vehicle. The analysis, based on the Chapman-Enskog method as applied by Shidlovskiy for a single-species gas, includes multicomponent diffusion with finite-rate surface catalytic recombination. A consistent set of equations is provided for multicomponent, binary, and single species mixtures.
Equations have been obtained for jump (or slip) in the wall values of species concentration, pressure, velocity, and temperature for the low-Reynolds-number high-altitude flight regime of a space vehicle. The analysis, based on the Chapman-Enskog method as applied by Shidlovskiy for a single-species gas, includes multicomponent diffusion with finite-rate surface catalytic recombination. A consistent set of equations is provided for multicomponent, binary, and single species mixtures.
Accuracy of scalar electrical conductivity calculations of partially ionized plasma using third Chapman-Enskog approximation method
Approximation method for thermal diffusion factor of almost Lorentzian gas mixture with better convergence properties than Chapman-Enskog approximation
Computer program for calculating classical and quantal JWKB Chapman-Enskog transport collision integrals with application to Morse potential
Thermoconductivity of fully and partially ionized gases based on heat flux vector expression in Chapman-Enskog formulation
Diffusion coefficients determination from viscosity measurements based on higher Chapman- Enskog approximations
Convergence of Chapman-Enskog approximations to scalar electrical conductivity of some weakly ionized real gases
Third Chapman-Enskog approximation to tensor electrical conductivity of partially ionized gas applied to two conductivity mixture rules for atmospheric cesium seeded argon
Lorentzian scalar electrical conductivity as basis of mixture rules proposed for partially ionized gases in magnetic field to calculate tensor conductivity
Chapman-Enskog transport collision integrals calculated for repulsive and attractive screened Coulomb potentials in ionized gases
Partially ionized He in chemical equilibrium at various pressures and temperatures, deriving transport coefficients with Chapman-Enskog- Burnett method
Method is derived from the Chapman-enskog theory which describes viscosities at low-to-moderate pressures. Mixtures of nonpolar gases require the viscosities and molecular weights of the constituents in addition to the mixture composition. Dipole moments, boiling points and liquid boiling point densities are also needed with polar gases.
Transport coefficients of partially ionized gas, using second order chapman-enskog formulation