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http://dx.doi.org/10.5139/JKSAS.2007.35.2.094

Numerical Analysis on Screech Tone in a Supersonic Jet  

Kim, Yong-Seok (순천대학교 기계우주항공공학부)
Lee, Duck-Joo (한국과학기술원 항공우주공학전공)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.35, no.2, 2007 , pp. 94-100 More about this Journal
Abstract
An axisymmetric supersonic jet screech in the Mach number range from 1.07 to 1.2 is numerically simulated. The axisymmetric mode is the dominant screech mode for an axisymmetric jet. The Reynolds-averaged Navier-Stokes equations in the conjunction with a modified Spalart-Allmaras turbulence model are employed. A high resolution finite volume essentially non-oscillatory(ENO) schemes are used along with nonreflecting characteristic boundary conditions that are crucial to screech tone computations to accurately capture the sound waves, shock-cell structures and large-scale instability waves.
Keywords
Supersonic jet flow; Screech tone; ENO schemes; Spalart-Allmaras turbulence model; axisymmetric modes;
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