2018
DOI: 10.1007/978-3-319-99719-3_20
|View full text |Cite
|
Sign up to set email alerts
|

Optimization of a Flanged DAWT Using a CFD Actuator Disc Method

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
6
0

Year Published

2019
2019
2023
2023

Publication Types

Select...
6

Relationship

3
3

Authors

Journals

citations
Cited by 6 publications
(6 citation statements)
references
References 12 publications
0
6
0
Order By: Relevance
“…For solving full-elliptic Navier-Stokes equations, k-ε and k-ω models were used. According to the previous studies [18,19,34], these two models can provide reliable results for flows around a rotor located in a duct. Two models were tested, and the k-ω model was selected [35].…”
Section: Geometry and Numerical Approach Of Duct Studymentioning
confidence: 85%
See 1 more Smart Citation
“…For solving full-elliptic Navier-Stokes equations, k-ε and k-ω models were used. According to the previous studies [18,19,34], these two models can provide reliable results for flows around a rotor located in a duct. Two models were tested, and the k-ω model was selected [35].…”
Section: Geometry and Numerical Approach Of Duct Studymentioning
confidence: 85%
“…In the study by Rochman et al [17], only the geometry of the flange of the duct was examined, which showed that adding a flat flange at the end of the duct causes an increase of 29% of wind speed in the throat region of the duct in comparison to the case without a flange. The studies of Ranjbar et al [18] and Al-Zahabi et al [19] focused only on the angle of a flange. Al-Zahabi et al showed that, for their selected geometry, by setting the angle of the flange at 15 degrees, the power coefficient can be increased up to 5%.…”
Section: Introductionmentioning
confidence: 99%
“…This technique has been widely applied and validated in different studies focused on the design of new models of ducted wind turbines [65][66][67][68][69]. With this aim, the Reynolds-Averaged Navier-Stokes (RANS) equations along with the k-ε turbulence model were solved by applying the finite-volume method [70][71][72]. Enhanced wall functions were used to model the airflow behaviour in the air region close to the solid surfaces.…”
Section: B Numerical Analysis Of the Patented Device Using Femmentioning
confidence: 99%
“…20 A flange added at the end of the shroud leads to an increase in the low back pressure of the shrouded turbine structure due to the formation of a strong vortex. 21,22 Also, as the last part of a shroud, a flange moves the maximum power coefficient toward large TSRs. 20,23 The length and angle of shrouds have been studied in other works.…”
Section: Introductionmentioning
confidence: 99%