Hostname: page-component-cd9895bd7-gxg78 Total loading time: 0 Render date: 2024-12-27T14:38:02.762Z Has data issue: false hasContentIssue false

Effects of exit Mach number and temperature on mean-flow and turbulence characteristics in round jets

Published online by Cambridge University Press:  20 April 2006

J. C. Lau
Affiliation:
Loekheed-Georgia Company, Marietta, Georgia U.S.A. Now with Kimberly-Clark Corporation, Neenah, Wisconsin, U.S.A.

Abstract

This paper describes mean-flow and turbulence measurements conducted in a round jet over a range of Mach numbers from 0·3 to 1·7 and jet-exit static temperatures from −40 to over 400 °C. It is a continuation of an earlier work, reported by Lau, Morris & Fisher (1979), to try to map the distribution of the various flow characteristics in the jet flow field and to observe the effects of changing jet exit conditions. In the earlier study, the effort was confined to isothermal jets at a limited number of exit Mach numbers, and the laser velocimeter proved to be a particularly useful instrument, especially in situations where the more severe flow conditions made it impossible to extract fluctuating-velocity data by any other means. The present effort capitalizes on this aspect of the velocimeter and also its ability to measure mean velocities accurately; and the extended range and detail of jet conditions chosen for this study is intended to provide a clearer understanding of the effects of systematically changing the jet conditions. Corresponding Pitot and total temperature measurements are also carried out under a representative set of jet conditions specifically to try to shed light on the effect of jet heating. Based on the various axial and radial distributions which are obtained, a picture is constructed of the changing boundaries of the shear layer with changing jet conditions.

Type
Research Article
Copyright
© 1981 Cambridge University Press

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Abramovich, G. N. 1963 The Theory of Turbulent Jets. Massachusetts Institute of Technology Press.
Barnett, D. O. & Giel, T. V. 1976 Arnold Engng Development Center Rep. no. AEDC-TR-76-36.
Batt, R. G. 1977 J. Fluid Mech. 82, 53.
Birch, S. F. & Eggers, J. M. 1972 N.A.S.A. SP-321, 11.
Bhadshaw, P., Ferris, D. H. & Johnson, R. E. 1964 J. Fluid Mech. 19, 591.
Cary, B. B. 1954 Ph.D. thesis, University of Maryland.
Corrsin, S. & Kistler, A. L. 1955 N.A.C.A. Rep. 1244.
Eggers, J. M. 1966 N.A.C.A. Tech. Note D-3601.
Korst, H. H. & Chow, W. L. 1962 Univ. of Illinois Mech. Eng. Rep. TN 393–2.
Lau, J. C. 1978 A.I.A.A. Paper no. 78–1152.
Lau, J. C. 1979 Proc. Roy. Soc. A 368, 547.
Lau, J. C. 1980 Laser velocimeter correlation measurements in subsonic and supersonic jets. J. Sound & Vib. 70, 85.Google Scholar
Lau, J. C., Morris, P. J. & Fisher, M. J. 1979 J. Fluid Mech. 93, 1. (See also 1976 A.I.A.A. Paper no. 76–348.)
Lau, J. C., Whiffen, M. C., Fisher, M. J. & Smith, D. M. 1981 J. Fluid Mech. 102, 353.
Tanna, H. K. 1977 J. Sound & Vib. 50, 405.
Whiffen, M. C., Lau, J. C. & Smith, D. M. 1979 Laser Velocimetry and Particle Sizing, Proc. 3rd Int. Workshop on Laser Velocimetry, Purdue Univ. 1978, p. 197. Hemisphere.
Witze, P. O. 1974 A.I.A.A. J. 12, 417.
Wygnanski, I. & Fiedler, H. 1969 J. Fluid Mech. 38, 577.