2016
DOI: 10.1080/09377255.2016.1205293
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Influence of propeller tip roughness on tip vortex strength and propeller performance

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Cited by 14 publications
(10 citation statements)
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“…With an increasing interest in Computational Fluid Dynamics (CFD), Krüger et al [32] investigated the effects of roughness on open water propeller performance under non-cavitating conditions using RANS and LES (Large Eddy Simulation) coupled with roughness model. The main aim of the study was to investigate the effects of propeller tip roughness and application area on the tip vortex pressure.…”
Section: Literature Reviewmentioning
confidence: 99%
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“…With an increasing interest in Computational Fluid Dynamics (CFD), Krüger et al [32] investigated the effects of roughness on open water propeller performance under non-cavitating conditions using RANS and LES (Large Eddy Simulation) coupled with roughness model. The main aim of the study was to investigate the effects of propeller tip roughness and application area on the tip vortex pressure.…”
Section: Literature Reviewmentioning
confidence: 99%
“…Results showed that with the rising number of bubbles at the beginning, there is an increase in the noise; however, there is a remarkable drop when the numbers of bubbles become larger for both roughened and smooth cases until 63Hz. Krüger et al [32] stated that Philipp and Ninnemann [37]`s study showed the application of roughness on a small area at the suction side of the blade close to the trailing edge could destabilise the tip vortex formation, hence its early breakdown. Cong et al [38] conducted an experimental study and tested the cavitation characteristics of a composite coating on a propeller.…”
Section: Literature Reviewmentioning
confidence: 99%
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“…However, the online version of record will be different from this version once it has been copyedited and typeset. PLEASE CITE THIS ARTICLE AS DOI:10.1063/5.0009622 [19] reported that suction-sided sand grain roughness reduces the tip vortex strength and leads to pressure increase in the vortex core. Souders and Platzer [20] discussed that the thicker turbulent boundary layer on the wing tip results in an increased tip vortex core radius and a decrease in the tip vortex maximum tangential velocity as compared to the laminar flow case.…”
Section: Introductionmentioning
confidence: 99%