2019
DOI: 10.1063/1.5084115
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Two-fluid plasma model for radial Langmuir probes as a converging nozzle with sonic choked flow, and sonic passage to supersonic flow

Abstract: Using the Lambert function, Guittienne et al. [Phys. Plasmas 25, 093519 (2018)] derived two-fluid solutions for radial Langmuir probes in collisionless and isothermal plasma. In this Brief Communication, we point out the close analogy with classical compressible fluid dynamics, where the simultaneous flows of the ion and electron fluids experience opposite electrostatic body forces in the inward radial flow of the plasma, which behaves as a converging nozzle. Hence, the assumed boundary condition of sonic flow… Show more

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Cited by 4 publications
(2 citation statements)
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“…A significant drop in temperature was observed as air comes out of the nozzle. It can possibly be related to the Joule-Thomson effect inducing temperature drops when high speed fluid quickly escapes through a narrow hole [29]. Static temperature drops during the isentropic expansion process and this drop in temperature is even more evident under supersonic flow where temperature can drop down to 213 K (−60 • C) without any cryogenic cooling or use of solid adsorption techniques [28].…”
Section: Resultsmentioning
confidence: 99%
“…A significant drop in temperature was observed as air comes out of the nozzle. It can possibly be related to the Joule-Thomson effect inducing temperature drops when high speed fluid quickly escapes through a narrow hole [29]. Static temperature drops during the isentropic expansion process and this drop in temperature is even more evident under supersonic flow where temperature can drop down to 213 K (−60 • C) without any cryogenic cooling or use of solid adsorption techniques [28].…”
Section: Resultsmentioning
confidence: 99%
“…However, the fibers became defective when pressure was further increased [100]. When air is passed through the air inlet and moves toward the nozzle tip, it must be ensured that there is no choking [101]. A nozzle is choked when the maximum mass flow rate has been reached [102].…”
Section: Air Pressure and Velocitymentioning
confidence: 99%