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Drag Reduction of a Circular Cylinder With O-rings

O-ring을 이용한 원주의 항력감소에 관한 실험적 연구

  • Published : 2003.08.01

Abstract

The flow around a circular cylinder was controlled by attaching O-rings to reduce drag force acting on the cylinder. Four experimental models were tested in this study; one smooth cylinder of diameter D (D=60mm) and three cylinders fitted with O-rings of diameters d=0.0167 D, 0.05D and 0.067 D with pitches of PPD=2D, 1D, 0.5D and 0.25D. The drag force, mean velocity and turbulence Intensity profiles in the near wake behind the cylinders were measured for Reynolds numbers based on the cylinder diameter in the range of Re$_{D}$=7.8$\times$10$^3$~1.2$\times$10$^{5}$ . At Re$_{D}$=1.2$\times$10$^{5}$ , the cylinder fitted with O-rings of d=0.0167D in a pitch interval of 0.25D shows the maximum drag reduction of about 5.4%, compared that with the smooth cylinder. The drag reduction effect of O-rings of d=0.067D is not so high. For O-ring circulars, as the Reynolds number increases, the peak location of turbulence intensity shifts downstream and the peak magnitude is decreased. Flow field around the cylinders was visualized using a smoke-wire technique to see the flow structure qualitatively. The size of vortices and vortex formation region formed behind the O-ring cylinders are smaller, compared with the smooth cylinder.der.

Keywords

References

  1. Cantwell, B. J., 1981, 'Organized Motion in Turbulent Flow,' Annual Rev. Fluid Mech., 13, pp. 457-515 https://doi.org/10.1146/annurev.fl.13.010181.002325
  2. Robinson, S. K., 1991, 'Coherent Motions in the Turbulent Boundary Layer,' Annual Rev. Fluid Mech., 23, pp. 601-639 https://doi.org/10.1146/annurev.fl.23.010191.003125
  3. Bandyopadhyay, P. R., 1986, 'Review - Mean Flow in Turbulent Boundary Layers Disturbed to Alter Skin Friction,' J. of Fluids Eng., Vol. 108, pp. 127-140 https://doi.org/10.1115/1.3242552
  4. Roshko, A., 'On the Drag and Shedding Frequency of Two-Dimensional Bluff Bodies,' National Advisory Committee for Aeronautics, NACA TN 3169
  5. Strykowski, P. J. and Sreenivasan, K. R., 1990, 'On the Formation and Suppressin of Vortex 'Shedding' at Low Reynolds Numbers,' J Fluid Mech., Vol 218, pp. 71-107 https://doi.org/10.1017/S0022112090000933
  6. Naudascher, E. and Rockwell, D., 1994, 'Flow-Induced Vibrations:An engineering Guide,' Rotterdam, A. A. Balkema Press
  7. Weaver, W., 1961, 'Wind-Induced Vibration in Antenna Members,' J. Eng. Mech. Div., Vol. 87, pp. 141-165
  8. Nebres, J. V., Batill, S. M., 1992, 'Flow about Cylinders with Helical Surface Protrusions,' 30th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, AIAA Paper 92-0540
  9. Zdravkovich, 1981, 'Review and Classification of Various Aerodynamics and Hydrodynamic Means for Suppressing Vortex Shedding,' J. Wind Engl. Ind. Aerodyn., Vol. 7, pp. 145-189 https://doi.org/10.1016/0167-6105(81)90036-2
  10. Lee, S. J., Kim, H. B., 1997, 'The Effect of Surface Protrusions on the Near Wake of a Circular Cylinder,' J. Wind Engl. Ind. Aerodyn., Vol.69, pp. 351-361 https://doi.org/10.1016/S0167-6105(97)00168-2
  11. Kwon, K. J., Kim, H. B. and Lee, S. J., 1996, 'Flow Characteristics of Near Wake behind a Circular Cylinder with Helical Surface Protrusions,' Trans. Of the KSME B, Vol.20(8), pp. 2601-2610
  12. Graham, J. M. R., 1969, 'The Effect of End-Plates on the Two-Dimensionality of a Vortex Wake,' Aero. Quart.,Vol.20, August, pp. 237-247 https://doi.org/10.1017/S0001925900005059
  13. Allen, H. J. and Vincenti, W. G., 1944, 'Wall Interference in A Two-Dimensional Flow and Wind Tunnel with Consideration of the Effect of Compressibility,' NACA, Wash., Rep. 782
  14. Stansby, P. K., 1974, 'The Effect of Endplates on the Base Pressure Coefficient of a Circular Circular Cylinder,' Aeronautical J., Vol. 78, pp. 36-37
  15. Wieselsberger, C., 'Neuere Feststellungen Uber die Gesetze des Flussigkeits - und Luftwiderstands,' Phys. Z. Vol. 22, 321-8