Hostname: page-component-7bb8b95d7b-fmk2r Total loading time: 0 Render date: 2024-09-06T10:22:58.843Z Has data issue: false hasContentIssue false

Interaction of impulsively generated vortex pairs with bodies

Published online by Cambridge University Press:  21 April 2006

J. Homa
Affiliation:
Department of Mechanical Engineering and Mechanics, Lehigh University, Bethlehem, PA 18015, USA
M. Lucas
Affiliation:
Department of Mechanical Engineering and Mechanics, Lehigh University, Bethlehem, PA 18015, USA
D. Rockwell
Affiliation:
Department of Mechanical Engineering and Mechanics, Lehigh University, Bethlehem, PA 18015, USA

Abstract

A vortex pair, impulsively generated from a planar nozzle, is shown to have a degree of vorticity concentration in good agreement with inviscid theory, providing well-posed initial conditions for interaction with basic types of bodies (cylinders and plates). The scale of these bodies ranges from the same order as, to over an order of magnitude smaller than, the scale (distance between centres) of the incident vortex pair.

The fundamental case of a (primary) vortex pair symmetrically incident upon a very small cylinder shows rapid growth of a secondary vortex pair. These secondary vortices quickly attain a circulation of the same order as that of the corresponding primary vortices within a distance smaller than the lengthscale of the primary vortex pair. At this location, the temporal variation of integrated vorticity of primary and secondary vortices attains a maximum simultaneously. This zero phase shift between arrival of vorticity maxima provides the basis for formation of counter-rotating, primary–secondary vortex pairs, where both the primary and secondary vortices move at the same phase speed.

Visualization shows that the mode of secondary vortex formation is highly sensitive to the degree of symmetry of the initial encounter of the incident vortex pair with the body. The symmetrical mode of (in-phase) secondary vortex formation shows very rapid growth of large-scale secondary vortices; their development is relatively independent of the particulars of body shape and scale. On the other hand, the antisymmetrical mode takes two basic forms: large-scale secondary vortex formation, with the phase shift between their formation determined by the lengthscale of the body; and small-scale, antisymmetrical shedding of secondary vortices from the body occurring for a body lengthscale an order of magnitude smaller than that of the incident vortex pair. Correspondingly, there are several types of distortion of the cores and trajectories of the primary (incident) vortices.

Type
Research Article
Copyright
© 1988 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

Batchelor, G. K.1967 An Introduction to Fluid Dynamics. Cambridge University Press.
Bushnell, D. M.1984 Body—turbulence interaction. AIAA Paper 84–1527. Presented at 17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference, June 25, 1984, Snowmass, Colorado.Google Scholar
Cerra, A. & Smith, C.1983 Experimental observations of vortex ring interaction with the fluid adjacent to the surface. Rep Fm-4, Lehigh University, AFOSR Tr-84–0130, 80A, No. 138999, 178 pp.
Didden, N. & Ho, C.-M. 1985 Unsteady separation in a boundary layer produced by an impinging jet. J. Fluid Mech. 160, 235256.Google Scholar
Doligalski, T. L., Smith, C. R. & Walker, J. D. A.1979 Production mechanism for turbulent boundary-layer flows. Symp. on Viscous Drag Reduction, Dallas, Texas, November 7–8.
Doligalski, T. L. & Walker, J. D. A.1984 Boundary layer induced by a convected two-dimensional vortex. J. Fluid Mech. 139, 128.Google Scholar
Harvey, J. K. & Perry, F. J.1971 Flow field produced by trailing vortices in the vicinity of the ground. AIAA J. 9, 15691616.Google Scholar
Ho, C.-M. 1983 An alternative look at the unsteady separation phenomenon. In Recent Advances in Aerodynamics, Proc. Int. Symp., Stanford University, August 22–26, pp. 165178, Springer.
Homa, J.1984 Interactions of an impulsively-generated two-dimensional vortex pair with flat plates and cylinders M.S. thesis, Department of Mechanical Engineering and Mechanics, Lehigh University, Bethlehem, Pa.
Homa, J. & Rockwell, D.1983 Vortex—body interaction. Bull. Am. Phys. Soc. 28, 1365.Google Scholar
Kaykayoglu, R. & Rockwell, D.1985 Vortices incident upon a leading-edge: instantaneous pressure fields. J. Fluid Mech. 156, 439461.Google Scholar
Kaykayoglu, R. & Rockwell, D.1986 Unstable jet—edge interaction. Part 1. Instantaneous pressure fields at a single frequency. J. Fluid Mech. 169, 125149.Google Scholar
Kiya, M., Ohyama, M. & Hunt, J. C. R.1986 Vortex pairs and rings interacting with shear layer vortices. J. Fluid Mech. 172, 117.Google Scholar
Lamb, H.1932 Hydrodynamics, 6th edn. p. 223. Dover.
Magarvey, R. H. & MacLatchy, C. S.1964 The disintegration of vortex rings. Can. J. Phys. 42, 684689.Google Scholar
Panaras, A. G.1985 Pressure pulses generated by the interaction of a discrete vortex with an edge. J. Fluid Mech. 154, 445462.Google Scholar
Panaras, A. G.1986 Simulation of impinging shear layers using vortex dynamics. AGARD/FDP, Round Table Discussion Aix-en-Provence, 10 April.
Panaras, A. G.1987 Numerical modelling of the vortex—airfoil interaction. AIAA J. 25, 511.Google Scholar
Rockwell, D.1983 Invited lecture: Oscillations of impinging shear layers. AIAA J. 21, 645664.Google Scholar
Rockwell, D.1984 Unsteady loading of leading-edges in unstable flows – an overview. AIAA Paper 84–2306Google Scholar
Schneider, P. E. M.1978 Morphologisch-phaenomenologische Unterschung der Umbildung von Ringwirbeln, die Koerper anstroemen. Rep. 14–1978, Max-Planck-Institut fuer Stroemungsforschung, Goettingen, West Germany.
Schneider, P. E. M.1980 Sekundaerwirbelbildung bei Ringwirbeln und in Freistrahlen. Z. Flugwiss. Weltraumforsch. 4, 307317.Google Scholar
Stuart, J. T.1967 On finite amplitude oscillations in laminar mixing layers. J. Fluid Mech. 29, 417440.Google Scholar
Sullivan, J. P., Widnall, S. E. & Ezekiel, S.1973 Study of vortex rings using a Laser-Doppler velocimeter. AIAA J. 11, 13841389.Google Scholar
Walker, J. D. A.1978 The boundary layer due to rectilinear vortex. Proc. R. Soc. Lond. A 350, 167188.Google Scholar
Ziada, S. & Rockwell, D.1982 Vortex—leading-edge interaction. J. Fluid Mech. 118, 79107.Google Scholar