Numerical study on the underexpanded Coanda jet

Kengo Asami, Keisuke Sawada

Research output: Contribution to conferencePaper

Abstract

The problem of Coanda jet flow in an underexpanded supersonic environment is studied numerically by solving the Navier-Stokes equations in two and three dimensions. The study considers a flow initiated by a jet bounded by a side wall and expanding around a circular cylinder, for which a set of experimental data exists. Two different turbulence models are used in the calculation, and the results are compared with the experimental data. In the two-dimensional calculation, the characteristic oscillatory pressure pattern is reproduced fairly well. The three-dimensional calculation reveals the influence of the side wall on the overall structure of the flow field.

Original languageEnglish
Pages1-9
Number of pages9
DOIs
Publication statusPublished - 1996 Jan 1
EventFluid Dynamics Conference, 1996 - New Orleans, United States
Duration: 1996 Jun 171996 Jun 20

Other

OtherFluid Dynamics Conference, 1996
CountryUnited States
CityNew Orleans
Period96/6/1796/6/20

ASJC Scopus subject areas

  • Mechanical Engineering
  • Fluid Flow and Transfer Processes
  • Energy Engineering and Power Technology
  • Aerospace Engineering

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  • Cite this

    Asami, K., & Sawada, K. (1996). Numerical study on the underexpanded Coanda jet. 1-9. Paper presented at Fluid Dynamics Conference, 1996, New Orleans, United States. https://doi.org/10.2514/6.1996-1936