한국전산유체공학회:학술대회논문집
- 2001.10a
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- Pages.84-90
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- 2001
Secondary Instability in the Wake of a Circular Cylinder
원주 후류에서의 2차적 불안정성
- KNAG S. J. ;
- TANAHASHI M. (Tokyo Institute of Technology Mechano-Aerospace Engineering) ;
- MIYAUCHI T. (Tokyo Institute of Technology Mechano-Aerospace Engineering) ;
- LEE Y. H.
- Published : 2001.10.01
Abstract
Secondary instability of flow past a circular cylinder is examined using direct numerical simulation at Reynolds number 220 and 250. The higher-order finite difference scheme is employed for the spatial distributions along with the second order Adams-Bashforth and the first order backward-Euler time integration. In x-y plane, the convection term is applied by the 5th order upwind scheme, and the pressure and viscosity terms are applied by the 4th order central difference. In spanwise, Navier-Stokes equation is distributed using Spectral Method. The critical Reynolds number for this instability is found to be about Re=190. The secondary instability leads re three-dimensionality with a spanwise wavelength about 4 cylinder diameters at onset (A-mode). Results of three-dimensional effect in wake of a circular cylinder are represented with spanwise and streamwise vorticity contours as Reynolds numbers.
Keywords