Hostname: page-component-cd9895bd7-hc48f Total loading time: 0 Render date: 2024-12-18T21:39:35.968Z Has data issue: false hasContentIssue false

On wavelike perturbations in a free jet travelling faster than the mean flow in the jet

Published online by Cambridge University Press:  29 March 2006

D. Bechert
Affiliation:
DFVLR-Institut für Turbulenzforschung, 1 Berlin 12. Müller-Breslau-Strasse 8
E. Pfizenmaier
Affiliation:
DFVLR-Institut für Turbulenzforschung, 1 Berlin 12. Müller-Breslau-Strasse 8

Abstract

The phase velocities of axial disturbances to a free jet have been investigated experimentally. For a certain range of low Strouhal numbers previous theories predicted the existence of phase velocities exceeding the mean velocity of the jet. These ‘ultra-fast’ phase velocities were found in the present experiments too.

Type
Research Article
Copyright
© 1975 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

Bechert, D. 1971a On some simplifications concerning calculations in aeroacoustics [in German]. DLR-FB 71-25.
Bechert, D. 1971b An aeroacoustic method for the calibration of hot-wire anemometers [in German]. Proc. 7th Int. Cong. on Acoustics, Budapest, paper 23N2.
Bechert, D. 1972 On multiple and upstream running waves in free jets [in German]. DLR-FB 72–06.
Bechert, D. & Michel, U. 1975 The control of a thin free shear layer with and without a semi-infinite plate by a pulsating flow field. Acustica, 33, 5 287.Google Scholar
Bechert, D. & Pfizenmaier, E. 1973 Optical compensation measurements on the unsteady exit condition at a nozzle discharge edge. An investigation in connexion with the sound transmission through nozzles with flow [in German]. DLR-FB 73–93.
Bechert, D. & Pfizenmaier, E. 1974 On wavelike perturbations in a free jet running faster than the mean flow of the jet [in German]. DLR-FB 74–26.
Bechert, D. & Pfizenmaier, E. 1975 Optical compensation measurements on the unsteady exit condition at a nozzle discharge edge. J. Fluid Mech. 71, 123.Google Scholar
Crow, S. C. & Champagne, F. H. 1971 Orderly structure in jet turbulence. J. Fluid Mech. 48, 547.Google Scholar
Freymuth, P. 1966 On transition in a separated laminar boundary layer. J. Fluid Mech. 25, 683.Google Scholar
Froebel, E. 1972 Instruction Manual of the DFVLR Hot-Wire Anemometer Mark HDA III [in German]. Berlin: DFVLR.
Michalke, A. 1961 Theoretical and experimental investigation of the laminar boundary layer of a circular nozzle [in German]. D. V. L. Rep. no. 177.Google Scholar
Michalke, A. 1969 The influence of the vorticity distribution on the inviscid instability of a free shear layer [ed. Polish Acad. Sci. Warsaw]. Fluid Dyn. Trans. 4, 751.Google Scholar
Michalke, A. 1970 A note on the spatial jet instability of the compressible cylindrical vortex sheet. DLR-FB 70–51.
Michalke, A. 1971 The instability of a compressible circular jet with finite boundary-layer thickness [in German]. Z. Flugwiss. 19, 319.Google Scholar
Miksad, R. W. 1972 Experiments on the nonlinear stages of free-shear-layer transition. J. Fluid Mech. 56, 695.Google Scholar
Orszag, S. A. & Crow, S. C. 1970 Instability of a vortex sheet, leaving a semi-infinite plate. Studies in Appl. Math. 49, 167.Google Scholar
Pfizenmaier, E. 1973 On the instability of the sound-influenced free jet [in German]. DLR-FB 73–69. (Trans. ESRO Tech. Trans. ESRO-TT-122.)