Abstract
Drag reduction in turbulent channel and pipe flows by spanwise (circumferential) wall oscillations is studied numerically. The influence of the wall oscillation on near-wall streamwise vortices is examined. By the use of the Stokes second problem, a wall-normal distance parameter and an acceleration parameter are obtained to estimate the drag reduction rate. A simple equation is derived for expressing the drag reduction rate by spanwise wall oscillations. The relation between near-wall streamwise vortices and low- and high-speed fluids is scrutinized to extract the key parameters. The drag reduction mechanism is analyzed in terms of the attenuation of Reynolds shear stress.
Original language | English |
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Pages (from-to) | 842-850 |
Number of pages | 9 |
Journal | AIAA journal |
Volume | 40 |
Issue number | 5 |
DOIs | |
Publication status | Published - 2002 May |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering