1971
DOI: 10.1063/1.1693336
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Flow Properties of a Partially Ionized Free Jet Expansion

Abstract: Diagnostic studies were carried out in an induction-heated low-density supersonic plasma jet. The neutral number densities were obtained from the calibrated intensity of the 4609-Å argon II line excited by a 25-kV electron beam, and the velocities and heavy particle temperatures were determined by measuring the Doppler shift and Doppler broadening with a Fabry-Perot interferometer in two linearly independent directions, following a technique developed by Muntz. The contribution to the 4609-Å line due to the pl… Show more

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Cited by 38 publications
(10 citation statements)
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“…The electron density also decreases with the square of the axial coordinate. [5][6][7][8][9][10][11][12][13][14][15] In Fig. 4 the experimental values and the modeling results show the same decrease.…”
Section: ͑21͒mentioning
confidence: 54%
“…The electron density also decreases with the square of the axial coordinate. [5][6][7][8][9][10][11][12][13][14][15] In Fig. 4 the experimental values and the modeling results show the same decrease.…”
Section: ͑21͒mentioning
confidence: 54%
“…It should be noted that no systematic studies of the gasdynamic structure of rarefied high-temperature jets have been performed at all. At present there are only single papers 15,16 containing data on the measurement of the total pressure and density in individual modes of flow, and studies of the physical processes in gas streams expanding from a plasma source have been conducted without the necessary attention to the gasdynamic structure of the jets.…”
Section: Gasdynamic Structure Of Low-density Plasma Jetsmentioning
confidence: 98%
“…Under typical conditions with the use of plasma heaters the degree of ionisation is small as a rule and does not exceed 1%. 16 The recombination coefficient is on the order of 10 -10 12 cm /s 21,22 and the relaxation rate is low. 23 This gives reason to assume that the ionisation in the jet is practically "frozen-in" and, consequently, the adiabatic index along a streamline corresponds to a monatomic gas.…”
mentioning
confidence: 99%
“…The stagnation temperature was calculated by using the simple choked flow relationship as given in [6]. Under our flow conditions, the Mach number was 4.0 at the nozzle exit and 4.4 at the blunt body position.…”
Section: Methodsmentioning
confidence: 99%