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An experimental and numerical study of the viscous stability of a round laminar vertical jet with and without thermal buoyancy for symmetric and asymmetric disturbances

Published online by Cambridge University Press:  29 March 2006

J. C. Mollendorf
Affiliation:
Engineering Research Center, Western Electric Co., Inc., Princeton, New Jersey
B. Gebhart
Affiliation:
Upson Hall, Cornell University, Ithaca, New York

Abstract

The fully viscous hydrodynamic stability equations for a round laminar vertical jet have been numerically solved using the proper boundary-layer base-flow velocity profile and for both symmetric and asymmetric disturbances. The symmetric mode is found to be unconditionally stable. The first asymmetric mode is found to be unstable and characteristics are compared with previous calculations. The computed critical Reynolds number for this mode is 9·4, which agrees with the calculations of Burridge (1968). Disturbance amplitude-ratio contours are also calculated and related to the convection of disturbances in the flow.

The effect of thermal buoyancy on jet stability is assessed by solving the fully viscous equations, coupled through buoyancy, and using a buoyancy-perturbed jet flow. A Prandtl number σ of 6·7 is used, and positive thermal buoyancy is found to have a destabilizing effect. Stability characteristics for the limiting case of buoyancy, a purely thermal point-source plume, are determined for a Prandtl number of 2.

Finally, an experiment was performed using water jets in water (σ ≈ 4·52–5·89) and a new method of jet production is described. The effect of varying amounts of thermal buoyancy on the laminar length of a jet undergoing naturally occurring transition was determined experimentally. These experiments confirm the calculated destabilizing effect of buoyancy. An empirical correlation is presented for the laminar length of a jet. Also, the effect of both symmetric and asymmetric artificially induced disturbances was determined experimentally. The disturbance amplitude ratio at which transition to turbulence takes place is found to be much less than for buoyant flows adjacent to a wall. The effects of frequency and amplitude of the artificial disturbances were experimentally determined and the trends are found to be consistent with the results of small disturbance theory.

The principal new result is that positive thermal buoyancy destabilizes jet flow, and consequently calls into question earlier experimental studies wherein jet flows were observed by density differences. Another new result is the calculation. of amplitude-ratio contours for a non-buoyant jet and the quantitative description of jet stability in terms of these contours along paths of constant physical frequency. A comparison of the non-buoyant theory with experimental jets containing varying amounts of thermal buoyancy indicates that transition did not occur at a well-defined value of the amplitude ratio. Perhaps experiments with truly non-buoyant jets and/or more detailed buoyant calculations could explain this remaining question.

Type
Research Article
Copyright
© 1973 Cambridge University Press

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References

Anderson, A. B. C. 1954 The jet-tone orifice number for orifices of small thicknessdiameter ratio. J. Acoust. Soc. Am. 26, 21.Google Scholar
Anderson, A. B. C. 1955 Structure and velocity of the periodic vortex-ring flow pattern of a primary Pfeifenton (pipe tone) jet. J. Acoust. Soc. Am. 27, 1048.Google Scholar
Anderson, A. B. C. 1956 Vortex-ring structure-transition in a jet emitting discrete acoustic frequency. J. Acoust. Soc. Am. 28, 914.Google Scholar
Batchelor, G. K. & Gill, A. E. 1962 Analysis of the stability of axisymmetric jets. J. Fluid Mech. 14, 529.Google Scholar
Becker, H. A. & Massaro, T. A. 1968 Vortex evolution in a round jet. J. Fluid Mech. 31, 435.Google Scholar
Burridge, D. M. 1968 The stability of round jets. Ph.D. thesis, Bristol University.
Crow, S. C. & Champagne, F. H. 1971 Orderly structure in jet turbulence. J. Fluid Mech. 48, 547.Google Scholar
Dring, R. P. & Gebhart, B. 1968 A theoretical investigation of disturbance amplification in external laminar natural convection. J. Fluid Mech. 34, 551.Google Scholar
Gebhart, B. & Knowles, C. P. 1966 Design and adjustment of a 20 cm Mach-Zehnder interferometer. Rev. Sci. Instrum. 37, 12.Google Scholar
Gill, A. E. 1962 On the occurrence of condensations in steady axisymmetric jets. J. Fluid Mech. 14, 557.Google Scholar
Hieber, C. A. & Gebhart, B. 1971 Stability of vertical natural convection boundary layers: some numerical solutions. J. Fluid Mech. 48, 625.Google Scholar
Kambe, T. 1969 The stability of an axisymmetric jet with parabolic profile. J. Phys. Soc. Japan, 26, 566.Google Scholar
Knowles, C. P. & Gebhart, B. 1968 The stability of the laminar natural convection boundary layer. J. Fluid Mech. 34, 657.Google Scholar
Landau, L. D. & Lifshitz, E. M. 1959 Fluid Mechanics, p. 86. Pergamon.
McKenzie, C. P. & Wall, D. B. 1968 Transition from laminar to turbulence in submerged and bounded jets. Fluidics Quart. 4, 38.Google Scholar
McNaughton, K. J. & Sinclair, C. G. 1966 Submerged jets in short cylindrical flowvessels. J. Fluid Mech. 25, 367.Google Scholar
Marsters, G. F. 1969 Some observations on the transition to turbulence in small, unconfined free jets. Queen's University, Kingston, Ontario, Rep. no. 1–69.Google Scholar
Mollendorf, J. C. 1971 The effect of thermal buoyancy on the hydrodynamic stability of a round laminar vertical jet. Ph.D. thesis, Cornell University.
Mollendorf, J. C. & Gebhart, B. 1973 Thermal buoyancy in round laminar vertical jets. Int. J. Heat Mass Transfer, 16, 735.Google Scholar
Pera, L. & Gebhart, B. 1971 On the stability of laminar plumes: some numerical solutions and experiments. Int. J. Heat Mass Transfer, 14, 975.Google Scholar
Reynolds, A. J. 1962 Observation of a liquid-into-liquid jet. J. Fluid Mech. 14, 552.Google Scholar
Schlichting, H. 1933 Laminare Strahlausbreitung. Z. angew. Math. Mech. 13, 260. (See also 1955 Boundary Layer Theory, p. 181. McGraw-Hill.)Google Scholar
Schuh, H. 1948 Boundary layers of temperature. W. Tollimien's Boundary Layers, B6. Brit. Min. Supply, German Document Centre, Ref. 3220T.
Squire, H. B. 1951 The round laminar jet. Quart. J. Mech. Appl. Math. 4, 321.Google Scholar
Vignes, M. 1968 Contribution à l’étude des jets gazeux verticaux dans une atmosphère calme. Rev. Gén. Thermique, 7, 1205.Google Scholar
Viilu, A. 1962 An experimental determination of the minimum Reynolds number for instability in a free jet. J. Appl. Mech. 29, 506.Google Scholar
Yih, C.-S. 1951 Free convection due to a point source of heat. Proc. 1st U.S. Nat. Conar. Appl. Mech. pp. 941947.Google Scholar