Analysis of the propeller wake by pressure and velocity correlation (Contributo in atti di convegno)

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Label
  • Analysis of the propeller wake by pressure and velocity correlation (Contributo in atti di convegno) (literal)
Anno
  • 2004-01-01T00:00:00+01:00 (literal)
Alternative label
  • M. Felli, F. Di Felice, G. Guj, R. Camussi (2004)
    Analysis of the propeller wake by pressure and velocity correlation
    in 15th Australasian Fluid Mechanics Conference, Sydney (AUS), 13-17 Dicembre 2004
    (literal)
Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#autori
  • M. Felli, F. Di Felice, G. Guj, R. Camussi (literal)
Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#url
  • http://www.aeromech.usyd.edu.au/15afmc/proceedings/papers/AFMC00124.pdf (literal)
Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#titoloVolume
  • Proceedings of the Fifteenth Australasian Fluid Mechanics Conference (literal)
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  • 4 (literal)
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  • 124 (literal)
Note
  • PuM (literal)
  • Google Scholar (literal)
Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#affiliazioni
  • INSEAN, Italian Institute for Naval Studies and Testing Department of Mechanical and Industrial Engineering \"Roma Tre\" University (literal)
Titolo
  • Analysis of the propeller wake by pressure and velocity correlation (literal)
Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#isbn
  • 1-864-87695-6 (literal)
Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#curatoriVolume
  • M. Behnia, W. Lin, & G. D. McBain (literal)
Abstract
  • In the present study an experimental analysis of the velocity and pressure fields behind a marine propeller, in non cavitating regime is reported. Velocity measurements were performed in phase with the propeller angle by using 2D Particle Image Velocimetry (2D-PIV). Measurements were carried out arranging the light sheet along the mid longitudinal plane of the propeller, to investigate the evolution of the axial and the radial velocity components, from the blade trailing edge up to 2 diameters downstream. The pressure measurements were performed at four radial and eight longitudinal positions downstream the propeller model. Measurements of the pressure field were performed at different advance ratios of the propeller. Pressure data, processed by using slotting techniques, allowed to reconstruct the evolution of the pressure field in phase with the reference blade position. In addition, the correlation of the velocity and pressure signals was performed. The analysis demonstrated that, within the near wake, the tip vortices passage is the most important contribution in generating the pressure field in the propeller flow. The incoming vortex breakdown process causes a strong deformation of the hub vortex far downstream the slipstream contraction. This process contributes to the pressure generation at the shaft rate frequency. (literal)
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