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  4. Development of an efficient CFD-based procedure with transitionsensitive turbulence model for evaluating the performance of marine propellers
 
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Development of an efficient CFD-based procedure with transitionsensitive turbulence model for evaluating the performance of marine propellers

Citation Link: https://doi.org/10.15480/882.9307
Publikationstyp
Conference Paper
Date Issued
2024-04-04
Sprache
English
Author(s)
Fouad, Mohamed Fathy  
Egyptian Armed Forces, Egypt
Kotb, Mohammed Abbas  
Alexandria University, Alexandria, Egypt
Abdel-Maksoud, Moustafa  orcid-logo
Fluiddynamik und Schiffstheorie M-8  
Moustafa, Moustafa Yasser  
Egyptian Armed Forces, Egypt
Ahmed, Tamer Mahmoud  
Alexandria University, Alexandria, Egypt
TORE-DOI
10.15480/882.9307
TORE-URI
https://hdl.handle.net/11420/46443
Start Page
615
End Page
624
Citation
8th International Symposium on Marine Propulsors (smp 2024)
Contribution to Conference
8th International Symposium on Marine Propulsors, smp 2024  
Publisher
Norwegian University of Science and Technology, Department of Marine Technology
ISBN
978-82-691120-5-4
Peer Reviewed
true
Is Part Of
10.15480/882.9294
In this paper, a CFD-based procedure for the evaluation of the performance characteristics of the well-known PPTC propeller, at model scale, is presented in detail. Results are obtained using one of the Local Correlation based Transition Models (LCTM), namely, the 𝛾 βˆ’π‘…π‘’Μƒ πœƒπ‘‘ transition model in combination with the π‘˜ βˆ’ πœ” SST turbulence model in a RANS-based numerical procedure to predict transition over the blade surface. The aim of using the 𝛾 βˆ’ 𝑅𝑒̃ πœƒπ‘‘ transition model is to predict the onset of transition and its influence on the propeller’s overall performance and on the flow behavior. Another aim of the work is to investigate the influence of the laminar-turbulent transition on the propeller’s flow. With the transition model, the constrained streamlines reflect an improvement in the flow pattern as compared to that of the model used for fully turbulent flow. Results also show an accurate prediction of the propeller’s global coefficients when the transition model is applied. Finally, a comparison between the results of the different transition models is conducted showing privilege of the 𝛾 βˆ’π‘…π‘’Μƒ πœƒπ‘‘ over other transition models in terms of predicting the overall performance of the propeller.
Subjects
CFD
PPTC Propeller
Transition-sensitive turbulence model
DDC Class
620: Engineering
Publication version
publishedVersion
Lizenz
http://rightsstatements.org/vocab/InC/1.0/
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