Hostname: page-component-cd9895bd7-dk4vv Total loading time: 0 Render date: 2024-12-20T05:36:08.632Z Has data issue: false hasContentIssue false
  • English
  • Français

The effects of yaw and finite length upon the vortex wakes of stationary and vibrating circular cylinders

Published online by Cambridge University Press:  20 April 2006

S. E. Ramberg
S. E. Ramberg
Affiliation:
Marine Technology Division, Naval Research Laboratory, Washington, DC 20375
Get access Rights & Permissions [Opens in a new window]

Abstract

The present investigation considers the vortex wakes behind finite-length yawed cylinders that are stationary or vibrating transversly in a uniform flow. In the Reynolds-number range 160–103 a number of three-dimensional and nominally two-dimensional wake flows are observed and attributed to the dominance of end conditions over rather large spans of the cylinder (aspect ratios up to 100).

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 128 , March 1983 , pp. 81 - 107
Copyright
© 1983 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

Bursnall, W. J. & Lofting, L. W. 1951 NACA TN 2463.
Chiu, W. S. 1966 Washington State University, College of Engineering Bulletin 299.
Dale, J. & Holler, R. A. 1970 USNADC Rep. AE-7011.
Davies, M. E. 1976 J. Fluid Mech. 75, 209–231.
Etzold, F. & Fiedler, H. 1976 Z. Flugwiss. 24, 77–82.
Fage, A. & Johansen, F. C. 1927 Proc. R. Soc. Lond A 116, 170–197.
Gerrard, J. H. 1966a J. Fluid Mech. 25, 143–164.
Gerrard, J. H. 1966b J. Fluid Mech. 25, 401–413.
Gerrard, J. J. 1978 Phil. Trans. R. Soc. Lond. A, 288, 351.
Graham, J. M. R. 1969 Aero. Q. 20, 237–247.
Griffin, O. M. 1971 Trans. A.S.M.E. E: J. Appl. Mech. 38, 729–738.
Griffin, O. M. 1978 J. Fluid Mech. 85, 591–607.
Griffin, O. M. 1981 Trans. A.S.M.E. I: J. Fluids Engng 103, 52–58.
Griffin, O. M. & Ramberg, S. E. 1974 J. Fluid Mech. 66, 553–576.
Griffin, O. M. & Ramberg, S. E. 1975 J. Fluid Mech. 69, 721–728.
Hanson, A. R. 1966 A.I.A.A. J. 4, 738–740.
King, R. 1977 Trans. A.S.M.E. I: J. Fluids Engng 99, 495–502.
Ramberg, S. E. 1978 Naval Research Lab. Memo. Rep. 3822.
Ramberg, S. E. & Griffin, O. M. 1974 Trans. A.S.M.E. I: J. Fluids Engng 96, 317–322.
Roshko, A. 1954a NACA Rep. 1191.
Roshko, A. 1954b NACA TN 3168.
Roshko, A. 1955 J. Aero. Sci. 22, 124–132.
Relf, E. H. & Powell, C. H. 1917 British A.R.C.
Schlichting, H. 1968 Boundary Layer Theory, 6th edn. McGraw-Hill.
Slaouti, A. & Gerrard, J. H. 1981 J. Fluid. Mech. 112, 297–314.
Smith, R. A., Moon, W. T. & Kao, T. W. 1972 Trans. A.S.M.E. D: J. Basic Engng 94, 711–776.
Stansby, P. K. 1974 Aero. J. 78, 36–37.
Van Atta, C. W. 1968 A.I.A.A. J. 6, 931–933.
Votaw, C. W. & Griffin, O. M. 1971 Trans. A.S.M.E. D: J. Basic Engng 93, 457–460.