2019
DOI: 10.1007/s40430-019-1822-8
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A CFD study on the correlation between the skew angle and blade number of hydrodynamic performance of a submarine propeller

Abstract: In the present study, the correlation between skew angle and blade number on the hydrodynamic performance of a submarine propeller is numerically investigated using computational fluid dynamics. For this purpose, three different blade numbers (3, 5 and 7 blades) and four different skew angles which vary from 0° to 52° are considered based on the INSEAN E1619 propeller model as the main geometry. Three-dimensional numerical simulation is based on Unsteady Reynolds-Averaged Navier-Stokes equations combined with … Show more

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Cited by 15 publications
(2 citation statements)
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“…Eskandarian and Liu 13 assessed numerically the propulsive performance of a helicopter propeller, and the influence of the blades' pitch on the maneuvering force and torque was cyclically obtained. Malmir 14 presented the effect of skew angle and blade number on the hydrodynamic performance and the propulsive efficiency of a submarine propeller by CFD, and was verified by a thrust experiment. Wu et al 15 numerically studied the hydrodynamic characteristics of the ducted propeller under yawing motion, and can demonstrate the thrust gradually increased in the wake of a speed incensement.…”
Section: Introductionmentioning
confidence: 94%
“…Eskandarian and Liu 13 assessed numerically the propulsive performance of a helicopter propeller, and the influence of the blades' pitch on the maneuvering force and torque was cyclically obtained. Malmir 14 presented the effect of skew angle and blade number on the hydrodynamic performance and the propulsive efficiency of a submarine propeller by CFD, and was verified by a thrust experiment. Wu et al 15 numerically studied the hydrodynamic characteristics of the ducted propeller under yawing motion, and can demonstrate the thrust gradually increased in the wake of a speed incensement.…”
Section: Introductionmentioning
confidence: 94%
“…For a propeller, the tip flow characterizes its wake topology. Without holding the propeller expansion area ratio, directly changing the blade number notably changes the performance [30][31][32] while the tip vorticity is not notably changed [31] as the load on per blade is not changed. Besides, the blade trailing wakes in propeller wake are restrained by increasing the skew angle [32,33].…”
Section: Introductionmentioning
confidence: 99%