On multi-point gas injection to form an air layer for frictional drag reduction. (1st January 2018)
- Record Type:
- Journal Article
- Title:
- On multi-point gas injection to form an air layer for frictional drag reduction. (1st January 2018)
- Main Title:
- On multi-point gas injection to form an air layer for frictional drag reduction
- Authors:
- Mäkiharju, Simo A.
Ceccio, Steven L. - Abstract:
- Abstract: Air layer drag reduction has been shown to be a feasible drag reducing technique at the laboratory and at full ship scales. In most studies, the air layers have been generated via gas injection from two-dimensional spanwise slots. However, given ship's structural considerations, it would be preferable to use discrete holes. The present study expands on the work on single orifice gas injection to multi-hole injection. When compared with slot injection, multi-point injection lead to a reduced range of gas fluxes that formed an air layer. Gas injected from a series of discrete holes can exhibit complex flow patterns, including roll-up into the core of liquid vortices that form as part of the process of injecting gas into the liquid boundary layer. The finite span and length of the model utilized for the present experiments was modest. It remains to be shown if a larger model with similar scaled up geometry (and with more beanwise holes) would enable the formation of a stable air layer with a gas flux per unit span that is similar to that required for slot injection. Nevertheless, the results presented here illustrate the complexity associated with gas injection through multiple perforations in a hull. Highlights: This study expands on the work on single orifice gas injection to multi-hole injection. Gas injected from a series of discrete holes to a liquid cross-flow can exhibit complex flow patterns. Compared with slot injection, multi-point injection lead to aAbstract: Air layer drag reduction has been shown to be a feasible drag reducing technique at the laboratory and at full ship scales. In most studies, the air layers have been generated via gas injection from two-dimensional spanwise slots. However, given ship's structural considerations, it would be preferable to use discrete holes. The present study expands on the work on single orifice gas injection to multi-hole injection. When compared with slot injection, multi-point injection lead to a reduced range of gas fluxes that formed an air layer. Gas injected from a series of discrete holes can exhibit complex flow patterns, including roll-up into the core of liquid vortices that form as part of the process of injecting gas into the liquid boundary layer. The finite span and length of the model utilized for the present experiments was modest. It remains to be shown if a larger model with similar scaled up geometry (and with more beanwise holes) would enable the formation of a stable air layer with a gas flux per unit span that is similar to that required for slot injection. Nevertheless, the results presented here illustrate the complexity associated with gas injection through multiple perforations in a hull. Highlights: This study expands on the work on single orifice gas injection to multi-hole injection. Gas injected from a series of discrete holes to a liquid cross-flow can exhibit complex flow patterns. Compared with slot injection, multi-point injection lead to a reduced range of gas fluxes that formed an air layer. … (more)
- Is Part Of:
- Ocean engineering. Volume 147(2018)
- Journal:
- Ocean engineering
- Issue:
- Volume 147(2018)
- Issue Display:
- Volume 147, Issue 2018 (2018)
- Year:
- 2018
- Volume:
- 147
- Issue:
- 2018
- Issue Sort Value:
- 2018-0147-2018-0000
- Page Start:
- 206
- Page End:
- 214
- Publication Date:
- 2018-01-01
- Subjects:
- Gas injection -- Multiphase -- Frictional drag reduction -- Air layer -- Jet
Ocean engineering -- Periodicals
Ocean engineering
Periodicals
620.4162 - Journal URLs:
- http://www.sciencedirect.com/science/journal/00298018 ↗
http://www.elsevier.com/journals ↗ - DOI:
- 10.1016/j.oceaneng.2017.10.041 ↗
- Languages:
- English
- ISSNs:
- 0029-8018
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 6231.280000
British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 18021.xml