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.

주제어

#압축성흐름   #바렐 충격파   #마하디스크   #충격파   #초음속노즐   #초음속 제트   #부족팽창 제트  

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이 논문을 인용한 문헌 (1)

1. Lee, Gwon-Hui ; Gu, Byeong-Su ; Kim, Hui-Dong 2001. "Study of the Flow Characteristics of Supersonic Coaxial Jets" 大韓機械學會論文集. Transactions of the Korean Society of Mechanical Engineers. B. B, 25(12): 1702~1710  원문보기 상세보기