2012
DOI: 10.5120/8841-3125
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CFD Analysis of a Propeller Flow and Cavitation

Abstract: The propeller is the predominant propulsion device used in ships. The performance of propeller is conventionally represented in terms of non-dimensional coefficients, i.e., thrust coefficient (K T ), torque coefficient (K Q ) and efficiency and their variation with advance coefficients (J). It is difficult to determine the characteristics of a full-size propeller in open water by varying the speed of the advance and the revolution rate over a range and measuring the thrust and torque of the propeller. Therefor… Show more

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Cited by 25 publications
(10 citation statements)
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“…8 that propeller 3 experienced the lowest efficiency. This is in correlation with Chang Sup Lee's prediction that increasing the expanded area ratio will cause the efficiency to decrease [14]. It can be seen from the Tables 10-12 that Propeller 3 consistently has the greatest K T for all values of J.…”
Section: Hydrodynamic Characteristicssupporting
confidence: 77%
See 3 more Smart Citations
“…8 that propeller 3 experienced the lowest efficiency. This is in correlation with Chang Sup Lee's prediction that increasing the expanded area ratio will cause the efficiency to decrease [14]. It can be seen from the Tables 10-12 that Propeller 3 consistently has the greatest K T for all values of J.…”
Section: Hydrodynamic Characteristicssupporting
confidence: 77%
“…A rotating region encapsulates the propeller and a static region covers the rest of the simulation domain. The dimensions of the two domains are comparable to Kutty and Rajendran [15], Subhas et al [14] and Tran Ngoc Tu [13] and provide a good foundation from which the current model is constructed. Tran Ngoc Tu compared different approaches to calculating propeller open water characteristics using the Reynolds Average Navier-Stokes (RANS) equations method.…”
Section: Introductionmentioning
confidence: 83%
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“…Subhas et al [16] performed a numerical study to study the performance of ship propeller by using CFD method, utilizing multiple reference frame (MRF) method. The results obtained were compared with experimental analysis, with maximum and minimum difference of 0.0013 and 0.001 respectively.…”
Section: Continuous Development and Optimization Of Unmannedmentioning
confidence: 99%