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Numerical Study of Characteristics of Underexpanded Supersonic Jet

Publication Type : Journal Article

Publisher : Journal of Aerospace Technology and Management

Source : Journal of Aerospace Technology and Management, SciELO Brasil, Volume 12 (2020)

Url : https://www.scielo.br/scielo.php?pid=S2175-91462020000100340&script=sci_arttext

Keywords : Numerical Analysis, Shock cell length, Supersonic core length, Supersonic jet

Campus : Coimbatore

School : School of Engineering

Department : Mechanical Engineering

Year : 2020

Abstract : Correlations for the supersonic jet characteristics, the mean shock cell length and the supersonic core length, have been obtained in terms of the jet parameters. The jet parameters considered in this study are the exit diameter of the nozzle (de), the design Mach number (Me), the nozzle pressure ratio (NPR) and the ratio of specific heats of the medium (γ). The parameters were varied as follows: exit diameters, from 0.5 to 25 mm; Mach number from 1 to 3; the NPR from 2.14 to 35. Initially, working fluid used is cold air and then effect of variation of γ is taken into consideration. The computational model has been validated and then used for all the numerical simulations. A quadratic fit for both characteristics has been obtained which is applicable to any supersonic jet. The correlations developed are valid within the respective ranges of the parameters stated above.

Cite this Research Publication : P. Murugesan, Kumar, A. Biju, Kambhampati, A. Teja, Pillai, S., Chandrasekar, G. Chandar, Raghavannambiar, S. Ambattu, and Dr. Ratna Kishore V., “Numerical Study of Characteristics of Underexpanded Supersonic Jet”, Journal of Aerospace Technology and Management, vol. 12, 2020.

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