2012
DOI: 10.1002/fld.3720
|View full text |Cite
|
Sign up to set email alerts
|

Application of the VORTFIND algorithm for the identification of vortical flow features around complex three‐dimensional geometries

Abstract: SUMMARYAccurate prediction of the hydrodynamic forces and moments acting on a manoeuvring marine vehicle using Reynolds Averaged Navier Stokes (RANS) simulations requires sufficient mesh resolution to capture offbody vortical structures. Since the path of these structures is not known a priori, a vortex identification and capture strategy is required alongside an iterative mesh adaption process. An improved version of the VORTFIND algorithm which can identify multiple vortices of variable strength and rotation… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

2016
2016
2022
2022

Publication Types

Select...
3

Relationship

0
3

Authors

Journals

citations
Cited by 3 publications
(2 citation statements)
references
References 29 publications
0
2
0
Order By: Relevance
“…Therefore, if you rank all the vectors by their proximity to different sectors you can determine how close they are to a vortex centre. This approach allows the position of a single vortex structure to be located and is simple to implement, but can be extended to cope with multiple vortex structures if required (Phillips and Turnock, 2013).…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, if you rank all the vectors by their proximity to different sectors you can determine how close they are to a vortex centre. This approach allows the position of a single vortex structure to be located and is simple to implement, but can be extended to cope with multiple vortex structures if required (Phillips and Turnock, 2013).…”
Section: Introductionmentioning
confidence: 99%
“…As shown in Figure 2, a relatively good agreement may be observed between the predicted and measured location of the cavitation regions. One of the drawbacks, however, is the lack of the tip vortex extending downstream of the propeller This is caused by lack of appropriate refinement of the mesh away from the propeller blade and by the fact that RANS methods in general tend to introduce too much dissipation and thus cause the vortices to disappear much sooner than they would in reality unless appropriate local mesh refinement is applied (Turnock et al, 2006, Phillips & Turnock., 2013.…”
Section: Resultsmentioning
confidence: 99%