Total thermal conductivity of partially and fully ionized gases.
Total thermoconductivity of ionized gas calculated with no simplification of components
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Total thermoconductivity of ionized gas calculated with no simplification of components
Previous calculations of thermal diffusion coefficients in partially ionized gases are extended to the case of unequal neutral and ion temperatures and/or temperature gradients. Formulas are derived for the general case of a major gas as well as for minor atoms and ions. Strong enhancements of minor-ion thermal diffusion coefficients over their values in the fully ionized gas are found when the degree of ionization in the main gas is relatively low. However, compared to the case of equal temperatures, the enhancements are less strong when the neutrals are cooler than the ions. The specific case of the H-H(+) mixture, which is important in the study of solar and stellar atmospheres, is discussed as an application.
Transport and thermodynamic properties of partially ionized gases
Chapman-Enskog transport collision integrals calculated for repulsive and attractive screened Coulomb potentials in ionized gases
Boltzmann equation used to derive the expression for the current in ionized gases at low density in an axisymmetric nonuniform field
Mass spectrometer for investigating composition of neutral and ionized gases in upper layers of atmosphere
Collisional theory of longitudinal wave propagation in partly ionized multitemperature gases
Particle diffusion distribution function of two component ionized degenerate gas from Boltzmann transport equation, giving tables for various spin and mass ratios
Spatially resolved He-Ne laser heterodyne measurements of electron number densities in weakly ionized Ar pulsed discharges
Magnetic field lines in a plasma reconnect at a rate scaled by the Alfven speed. In a partially ionized gas there are two natural Alfven speeds: one determined by the ionized mass density alone, which applies when ion-neutral friction is negligible, and one determined by the total mass density, which applies when ion-neutral friction is strong. When the ionization fraction is low, as in a dense molecular cloud, these two speeds differ by several orders of magnitude. Both time-dependent tearing modes and steady-state magnetic reconnection in partially ionized gas are considered, and the regimes in which the charged and neutral components are strongly, intermediately, and weakly coupled are delineated. Molecular clouds are probably in the intermediate regime, while reconnection in solar prominences probably has strong ion-neutral coupling. Reconnection proceeds more rapidly when coupling is not strong.
We have begun a comprehensive series of analyses and experiments to study the basic problem of shock wave dynamics in ionized media. Our objective is to isolate the mechanisms that are responsible for the decrease in the shock amplitude and also to determine the relevant plasma parameters that will be required for a drag reduction scheme in an actual high altitude hypersonic flight. Specifically, we have initiated a program of analyses and measurements with the objective of (i) fully characterizing the propagation dynamics in plasmas formed in gases of aerodynamic interest, (ii) isolating the mechanisms responsible for the decreased shock strength and increased shock velocity, (iii) extrapolating the laboratory observations to the technology of supersonic flight.
Two areas of research are briefly summarized. The first is concerned with calculating the conductivity of a slightly ionized gas. A method is proposed which involves an expansion of the Boltzmann collision operator (of the electron distribution function, involving the neutral gas-electron interactions) in powers of the electron-gas mass ratio. The second area of investigation focuses on the problem of a radio wave propagating through the interplanetary medium, taking account of the decreasing plasma density with distance from the sun.
Based on previous laminar boundary-layer solutions for argon, xenon, nitrogen, and air, it is shown that the effect of gas ionization on stagnation-point heat transfer can be correlated with the variation of the frozen Prandtl number across the boundary layer. A formula is obtained for stagnation-point heat transfer in a noble gas and is shown to be valid from the low-temperature range to the region of strong ionization. It is concluded that the considered effect can be well correlated by the 0.7 power of the Prandtl-number ratio across the boundary layer.
Boltzmann equation expressions for electric current in plasma at low density in magnetic field
Summaries and reviews of conference papers on electron-atom collision theory
Gas dynamics of nonequilibrium flows of plasmas and dissociated gases, discussing nozzle and corner expansion flows
Transport properties for weakly ionized gases, binary Maxwell molecular gases, and fully ionized gases