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Vortex shedding from a cylinder vibrating in line with an incident uniform flow

Published online by Cambridge University Press:  29 March 2006

Owen M. Griffin  and
Steven E. Ramberg
Owen M. Griffin
Affiliation:
Naval Research Laboratory, Washington, D.C. 20375
Steven E. Ramberg
Affiliation:
Naval Research Laboratory, Washington, D.C. 20375
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Abstract

A study has been made of the wake of a cylinder vibrating in line with an incident steady flow. The Reynolds number for the experiments was 190, and the vortex shedding was at all times synchronized with the vibrations of the cylinder, which were in a range of frequencies near twice the Strouhal shedding frequency for the stationary cylinder. Two distinct vortex wake patterns were encountered. The first is a complex regime in which two vortices are shed during each cycle of the vibration and form an alternating pattern of vortex pairs downstream. The second pattern is an alternating street which results from the shedding of a single vortex during each cycle of the cylinder's motion. The street geometry in the latter case shares many basic characteristics with the wake of a cylinder vibrating in cross-flow. These include the effects of vibration amplitude and frequency on the longitudinal and transverse spacing of the vortices. The results obtained from these experiments in air are in agreement with previous findings from free- and forced-vibration experiments in water at both higher and lower Reynolds numbers.

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 75 , Issue 2 , 27 May 1976 , pp. 257 - 271
Copyright
© 1976 Cambridge University Press

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References

Berger, E. W. & Wille, R. 1972 Ann. Rev. Fluid Mech. 4, 313–810.
Christiansen, J. P. & Zabusky, N. 1973 J. Fluid Mech. 61, 219–810.
Gbiffin, O. M. 1971 Trans. A.S.M.E., J. Appl. Mech. 38, 729–810.
Griffin, O. M. & Ramberg, S. E. 1974 J. Fluid Mech. 66, 553–810.
Griffin, O. M. & Ramberg, S. E. 1975 J. Fluid Mech. 69, 721–810.
Griffin, O. M., Ramberg, S. E., Votaw, C. W. & Kelleher, M. D. 1973 Proc. Int. Cong. Instrumentation in Aerospace Simulation Facilities (IEEE), pp. 133–139.
Griffin, O. M., Skop, R. A. & Ramberg, S. E. 1975 Offshore Tech. Conf., Houston, paper OTC 2319.
Griffin, O. M. & Votaw, C. W. 1972 J. Fluid Mech. 55, 31–810.
King, R. 1974 Offshore Tech. Conf., Houston, paper OTC 1948.
King, R., Prosser, M. J. & Johns, D. J. 1973 J. Sound Vib. 29, 169–810.
Koopmann, G. H. 1967 J. Fluid Mech. 28, 501–810.
Mair, W. A. & Maull, D. J. 1971 J. Fluid Mech. 45, 209–810.
NAUDASCHER, E. (ed.) 1974 Flow-Induced Structural Vibrations, pp. 587–601. Springer.
Parkinson, G. V. 1971 Phil. Trans A 229, 395–409.
Ramberg, S. E. & Griffin, O. M. 1976 Trans. A.S.M.E., J. Fluids Engng, 98, 10–810.
Sainsbury, R. & King, N. 1971 Proc. Inst. Civil Engrs, 49, 269–810.
Tanida, Y., Okajima, A. & Watanabe, Y. 1973 J. Fluid Mech. 61, 769–810.
Tatsuno, M. 1972 Bull. Res. Inst. Appl. Mech., Kyushu University, 36, 25–810 (in Japanese).
Twigge-Molecey, C. F. M. & Baines, W. D. 1973 Proc. A.S.C.E., J. Engng Mech. 99, 803–810.
Wootton, L. R., Warner, M. H., Sainsbury, R. N. & Cooper, D. H. 1972 Construction Indust. Res. & Inf. Ass. Land. Rep. CIRIA 41.