Comptes Rendus
A mean flow field solution to a moderately under/over-expanded turbulent supersonic jet
[Une solution à champ d'ècoulement moyen pour un jet supersonique turbulent modérément sous/sur-expansé]
Comptes Rendus. Mécanique, Volume 337 (2009) no. 4, pp. 185-191.

La solution linéarisée pour un jet à la fois axisymétrique, supersonique, non-visqueux et imparfaitement expansé a été portée au cas d'un ècoulement turbulent en tenant compte des contraintes Reynolds moyennes. Les résultats analytiques correspondent plutôt bien aux données expérimentales disponibles dans la literature. Ils indiquent donc que la solution est une bonne approximation au quasi-champ d'un jet imparfaitement expansé. Cette solution analytique pourrait servir à améliorer les modéles semi-empiriques de bruits de large bande liés aux chocs dans de domaine de l'aéronautique.

The linearized solution for an inviscid imperfectly-expanded supersonic axisymmetric jet has been extended to the case of a turbulent flow, by taking into account the mean Reynolds stresses. The analytical results agree reasonably well with experimental data available in the literature, and so indicate that the solution is a good approximation to the near-field of an imperfectly-expanded jet. This analytical solution could be used to improve semi-empirical models of broadband shock-associated noise in aeronautics.

Reçu le :
Accepté le :
Publié le :
DOI : 10.1016/j.crme.2009.05.002
Keywords: Analytical solution, Supersonic, Jet
Mot clés : Solution analytique, Supersonique, Jet
Babak Emami 1 ; Markus Bussmann 1 ; Honghi N. Tran 2

1 Department of Mechanical and Industrial Engineering, University of Toronto, Toronto, ON M5S 3G8, Canada
2 Department of Chemical Engineering and Applied Chemistry, University of Toronto, Toronto, ON M5S 3E5, Canada
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Babak Emami; Markus Bussmann; Honghi N. Tran. A mean flow field solution to a moderately under/over-expanded turbulent supersonic jet. Comptes Rendus. Mécanique, Volume 337 (2009) no. 4, pp. 185-191. doi : 10.1016/j.crme.2009.05.002. https://comptes-rendus.academie-sciences.fr/mecanique/articles/10.1016/j.crme.2009.05.002/

[1] A. Pophali; A. Kaliazine; D.E. Cormack; H.N. Tran Visualization of supersonic air jets using high-speed Schlieren technique, 20th Annual Meeting of the Consortium on Increasing Energy and Chemical Recovery in the Kraft Pulping Process, University of Toronto, Canada, 2007

[2] D.C. Pack A note on Prandtl's formula for the wave-length of a supersonic gas jet, Quart. J. Mech. Appl. Math., Volume 3 (1950), pp. 173-181

[3] M.S. Howe; J.E. Ffowcs-Williams On the noise generated by an imperfectly-expanded supersonic jet, Philos. Trans. Roy. Soc. London Ser. A, Volume 289 (1978) no. 1358, pp. 271-314

[4] C.K.W. Tam On the noise of a nearly ideally expanded supersonic jet, Fluid Mech., Volume 51 (1972) no. 1, pp. 69-95

[5] J. Panda Shock oscillation in under-expanded screeching jets, J. Fluid Mech., Volume 363 (1998), pp. 173-198

[6] C.K.W. Tam; J.A. Jackson; J.M. Seiner A multiple-scales model of the shock-cell structure of imperfectly-expanded supersonic jets, J. Fluid Mech., Volume 153 (1985), pp. 123-149

[7] G. Kleinstein Mixing in turbulent axially symmetric free jets, J. Spacecraft, Volume 1 (1964) no. 4, pp. 403-408

[8] P.O. Witze Centerline velocity decay of compressible free jets, AIAA J., Volume 12 (1974) no. 4, pp. 416-418

[9] S.E. Selezneva; M. Rajabian; D. Gravelle Study of the structure and deviation from equilibrium in direct current supersonic plasma jets, J. Phys. D: Appl. Phys., Volume 34 (2001) no. 18, pp. 2862-2874

[10] J.M. Seiner, T.D. Norum, Aerodynamic aspects of shock containing jet plumes, AIAA Paper 80-0965, 1980

[11] T.D. Norum, J.M. Seiner, Measurements of mean static pressure and far-field acoustics of shock containing supersonic jets, NASA Technical Memorandum 84521, 1982

[12] J. Panda; R.G. Seasholtz Measurement of shock structure and shock-vortex interaction in under-expanded jets using Rayleigh scattering, Phys. Fluids, Volume 11 (1999) no. 12, pp. 3761-3777

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