Hostname: page-component-848d4c4894-nmvwc Total loading time: 0 Render date: 2024-06-23T15:19:07.824Z Has data issue: false hasContentIssue false

Experiments on the trajectory and circulation of the starting vortex

Published online by Cambridge University Press:  21 April 2006

David Auerbach
Affiliation:
Max Planck-Institut für Strömungsforschung, Bunsenstr. 10, D-3400 Göttingen, Federal Republic of Germany

Abstract

Various reasons have been given as to why the trajectories and circulations of vortices generated at sharp edges do not follow classical similarity-theory predictions for at least an initial short time. Amongst these are the effect of the particular flow geometry (e.g. duct with wedge, nozzle) distant from the salient edge (for rectilinear vortices); axisymmetry (for ring vortices); end effects (for rectilinear vortices); viscous diffusion; finite thickness of the detaching shear layer, as well as secondary vorticity caused by the interaction of the primary vortex with the edge at which it was generated. A further process that may be active is that of viscous entrainment. Experiments, in which essentially straight-line vortices were generated, indicate that of the seven possibilities mentioned, the first five do not play a significant part. All models consist of a basic flow onto which the modelled vortex is superposed. Thus either the basic flow or the vortex model are at fault. The basic flow onto which the vortex is superposed may well not be a pure edge flow, but one that is already taking on the character of an entraining jet flow. On the other hand, the vortex model fails to incorporate secondary vorticity which, particularly when rolled up, might be expected to be dynamically important.

Type
Research Article
Copyright
© 1987 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

Auerbach, D. E. 1987 Some three-dimensional effects during vortex generation at a straight edge. Exp. Fluids (in press).Google Scholar
Blondeaux, P. & De Bernadinis, B. 1983 On the formation of vortex pairs near orifices. J. Fluid Mech. 135, 111122.Google Scholar
Bossel, H. H., Hiller, W. J. & Meier, G. E. A. 1972 Noise-cancelling signal difference method for optical velocity measurements. J. Phys. E: Sci. Instrum. 5, 8931096.Google Scholar
Brown, C. E. & Michael, W. H. 1955 On slender delta wings with leading edge separation. NACA Tech. Note 3430.
Chow, C.-Y. & Huang, M.-K. 1982 The initial lift and drag of an impulsively started aerofoil of finite thickness. J. Fluid Mech. 118, 393409.Google Scholar
Didden, N. 1977 Untersuchung laminarer, instabiler Ringwirbel mittels Laser-Doppler-Anemometrie. MPI/AVA Bericht 64.
Didden, N. 1979 On the formation of vortex rings: rolling-up and production of circulation. Z. Angew. Math. Phys. 30, 101115.Google Scholar
Didden, N. 1982 On vortex formation and interaction with solid boundaries. In Vortex Motion (ed. H. G. Hornung & E.-A. Müller), pp. 117. Braunschweig: Vieweg.
Graham, J. M. R. 1977 Vortex shedding from sharp edges. IC Aero-Rep. 77–01. Imperial College of Science and Technology.
Graham, J. M. R. 1983 The lift on an aerofoil in starting flow. J. Fluid Mech. 133, 413425.Google Scholar
Kaden, H. 1931 Aufwicklung einer unstabilen Unsetigkeitsfläche. Ing.-Arch. 2, 140168.Google Scholar
Kraemer, K. 1971 Die Potentialströmung in der Umbgebung von Freistrahlen. Z. Flugwiss. 19, 94104.Google Scholar
Pullin, D. I. 1978 The large-scale structure of unsteady self-similar rolled-up vortex sheets. J. Fluid Mech. 88, 401430.Google Scholar
Pullin, D. I. 1979 Vortex generation at tube and orifice openings. Phys. Fluids 22, 401403.Google Scholar
Pullin, D. I. & Perry, A. E. 1980 Some flow visualization experiments on the starting vortex. J. Fluid Mech. 97, 239255.Google Scholar
Taylor, G. I. 1958 Flow induced by jets. J. Aero/Space Sci. 25, 464465.Google Scholar
Walker, J. D. A. 1978 The boundary layer due to a rectilinear vortex. Proc. R. Soc. Lond. A 359, 167188.Google Scholar
Wedemeyer, E. 1961 Ausbildung eines Wirbelpaares an den Kanten einer Platte. Ing.-Arch. 30, 187200.Google Scholar