Direct current thermal plasma jets are strongly affected on the one hand by the arc root fluctuations at the anode, resulting in a type of pulsed flow and enhanced turbulence, and on the other hand by the entrainment of surrounding cold gas in the plasma jet. These phenomena and the resulting temperature distributions have been studied using a wide range of diagnostic techniques, including fast cameras, laser doppler anemometry (LDA), coherent anti-Stokes Raman spectroscopy (CARS), Rayleigh scattering, emission spectroscopy, Schlieren photography, enthalpy probes, and sampling probes. The information obtained by these techniques is evaluated and compared. The effect of the arc fluctuations on the spectroscopic measurements is emphasized, and the possibility of using these fluctuations to determine information on the arc behavior and the axial velocity of the jet is presented. Optimization of plasma processing of solid particles requires information about their size and surface temperature, as well as number flux, and velocity distributions at various locations in the flow field. The different statistical techniques of inflight measurements are discussed together with their limitations. A method to determine the temperature and species density of the vapor cloud or comet traveling with each particle in flight is then presented. However, such statistical measurements present ambiguities in their interpretation, which can be addressed only by additional measurements to determine the velocity, diameter, and surface temperature of a single particle in flight. Moreover, information on single particles is required to understand the coating properties, which depend strongly on the way the particles flatten and solidify upon impact. A method to obtain data related to a single particle in flight and to follow the temperature evolution of the corresponding splat upon cooling is presented. The article concludes with the description of the experimental techniques to follow the temperature evolution of the successive layers and passes. This is important because temperature distribution within the coating and substrate controls the adhesion and cohesion of coatings as well as their residual stress.
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