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Numerical Study on Under-Expanded Jets through a Supersonic Nozzle(II)
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 Title & Authors
Numerical Study on Under-Expanded Jets through a Supersonic Nozzle(II)
Kim, Hui-Dong; Sin, Hyeong-Seung;
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 Abstract
Numerical calculation was applied to supersonic under-expanded jets, and compared with the results of a linear theory and other experiments. TVD difference scheme was employed to solve 2-dimensional and axisymmetric inviscid Euler equation. This paper aims to explore the effects of angle of divergence and design Mach number of nozzle on the structure of under-expanded jets. The angle of divergence was varied from 0 to 20 deg. The results show that the length of the first cell of the under-expanded jets decreases and Mach disk generates at lower nozzle pressure ratio, if the angle of divergence or design Mach number of nozzle increases. The distance from the nozzle exit to Mach disk in 2-dimensional jets becomes much larger than that of axisymmetric jets, and the widths of the jet boundary and the barrel shock wave are also larger than that of axisymmetric jets. Calculation results indicate that the configuration of the under-expanded jets is strongly dependent on the nozzle pressure ratio.
 Keywords
Compressible Flow;Barrel Shock Wave;Mach Disk;Shock Wave;Supersonic Nozzle;Supersonic Jet;Under-Expanded Jet;
 Language
Korean
 Cited by
1.
초음속 동축제트의 유동특성에 관한 연구,이권희;구병수;김희동;

대한기계학회논문집B, 2001. vol.25. 12, pp.1702-1710 crossref(new window)
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