Vorticity modification in a turbulent channel flow by micro-bubble injection
- 1. Mechanical Engineering Department, Texas University, College Station (United States)
- 2. Nuclear Engineering Department, Texas University, College Station (United States)
Description
Investigation of the drag reduction phenomenon has been carried out for several years. Several techniques to reduce the drag have been applied and researched for a number of years. Micro-bubbles injection within a turbulent boundary layer is one method utilized to achieve reduction of drag. In this paper, the results for vorticity modification by injection of micro-bubbles are presented and discussed. The experimental velocity field results were obtained using particle image velocimetry in an x-y plane located close to the wall. Micro-bubbles presence within the boundary layer produces a decrease in the z-vorticity component. This is a consequence of a decrease in the wall shear stress. The decrease of the vorticity in the near-wall region also indicates a decrease in strain, which leads to a suppression of the Reynolds stresses. All of these changes lead to a decrease in drag
Additional details
Publishing Information
- Publisher
- American Society of Mechanical Engineers - ASME
- Imprint Place
- New York (United States)
- ISBN
- 0-7918-4687-3
- Imprint Title
- Proceedings of the 12. international conference on nuclear engineering
- Imprint Pagination
- 924 p.
- Journal Page Range
- p. 851-854
Conference
- Title
- 12. international conference on nuclear engineering - ICONE 12
- Dates
- 25-29 Apr 2004
- Place
- Arlington - Virginia (United States)
INIS
- Country of Publication
- United States
- Country of Input or Organization
- France
- INIS RN
- 37113742
- Subject category
- S42: ENGINEERING;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- BOUNDARY LAYERS; BUBBLES; DRAG; MINIMIZATION; SHEAR; TURBULENCE; TURBULENT FLOW; VORTICES
- Descriptors DEC
- FLUID FLOW; LAYERS; OPTIMIZATION
Optional Information
- Notes
- 7 refs.