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Instantaneous and time-averaged flow fields of multiple vortices in the tip region of a ducted propulsor

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Abstract

The instantaneous and time-averaged flow fields in the tip region of a ducted marine propulsor are examined. In this flow, a primary tip-leakage vortex interacts with a secondary, co-rotating trailing edge vortex and other co- and counter-rotating vorticity found in the blade wake. Planar particle imaging velocimetry (PIV) is used to examine the flow in a plane approximately perpendicular to the mean axis of the primary vortex. An identification procedure is used to characterize multiple regions of compact vorticity in the flow fields as series of Gaussian vortices. Significant differences are found between the vortex properties from the time-averaged flow fields and the average vortex properties identified in the instantaneous flow fields. Variability in the vortical flow field results from spatial wandering of the vortices, correlated fluctuations of the vortex strength and core size, and both correlated and uncorrelated fluctuations in the relative positions of the vortices. This variability leads to pseudo-turbulent velocity fluctuations. Corrections for some of this variability are performed on the instantaneous flow fields. The resulting processed flow fields reveal a significant increase in flow variability in a region relatively far downstream of the blade trailing edge, a phenomenon that is masked through the process of simple averaging. This increased flow variability is also accompanied by the inception of discrete vortex cavitation bubbles, which is an unexpected result, since the mean flow pressures in the region of inception are much higher than the vapor pressure of the liquid. This suggests that unresolved fine-scale vortex interactions and stretching may be occurring in the region of increased flow variability.

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References

  • Arndt REA (2002) Cavitation in vortical flows. Annu Rev Fluid Mech 34:143–175

    Google Scholar 

  • Baker GR, Barker SJ, Bofah KK, Saffman PG (1974) Laser anemometer measurements of trailing vortices in water. J Fluid Mech 65:325–336

    Google Scholar 

  • Balzani N, Scarano F, Riethmuller ML, Breugelmans FAE (2000) Experimental investigation of the blade-to-blade flow in a compressor rotor by digital particle image velocimetry. ASME J Turbomachinery 122:743–750

    Google Scholar 

  • Boulon OB, Callenaera M, Franc J-P, Michel J-M (1999) An experimental insight into the effect of confinement on tip vortex cavitation of an elliptic hydrofoil. J Fluid Mech 390:1–23

    Google Scholar 

  • Brennen CE (1995) Cavitation and bubble dynamics. Oxford University Press, Oxford

    Google Scholar 

  • Chen AL, Jacob JD, Savas Ö (1999) Dynamics of corotating vortex pairs in the wakes of flapped airfoils. J Fluid Mechanics 382:155–193

    Google Scholar 

  • Chesnakas C, Jessup S (2003) Tip vortex induced cavitation on a ducted propulsor. In: Proceedings of the 4th ASME-JSME joint fluids engineering conference, Honolulu, Hawaii, July 2003, FEDSM2003–45320

  • Chow YC, Uzol O, Katz J, Meneveau C (2002) An investigation of axial turbomachinery flows using PIV in an optically-unobstructed facility. In: Proceedings of the 9th international symposium on transport phenomena and dynamics of rotating machinery, Honolulu, Hawaii, February 2002

  • Copland CM, Coton FN, Galbraith RA (1998) An experimental study on the idealised vortex system of a novel rotor blade tip. Aeronautical J 102(1017):385–392

    Google Scholar 

  • Day KM, Lawless P, Fleeter S (1996) Particle image velocimetry measurements in a low speed research turbine. AIAA paper no. 96–2569

  • Devenport WJ, Rife MC, Liapis SI, Follin G (1996) The structure and development of a wing-tip vortex. J Fluid Mech 312:67–106

    Google Scholar 

  • Devenport WJ, Zsoldos JS, Vogel CM (1997) The structure and development of a pair of counter-rotating wing-tip vortices. J Fluid Mech 332:71–104

    CAS  Google Scholar 

  • Devenport WJ, Vogel CM, Zsoldos JS (1999) Flow structure produced by the interaction and merger of a pair of co-rotating wing-tip vortices. J Fluid Mech 394:357–377

    Google Scholar 

  • Farrell KJ, Billet ML (1994) A correlation of leakage vortex cavitation in axial-flow pumps. J Fluids Eng 116:551–557

    Google Scholar 

  • Figliola RS, Beasley DE (2000) Theory and design for mechanical measurements, 3rd edn. Wiley, New York, pp 132–138

    Google Scholar 

  • Fouras A, Soria J (1998) Accuracy of out-of-plane vorticity measurements derived from in-plane velocity field data. Exp Fluids 25:409–430

    Article  Google Scholar 

  • Gogineni S, Goss L, Copenhaver W, Gorrell S (1997) Development of digital two-color PIV for turbomachinery applications. AIAA paper no. 97–0494

  • Gopalan S, Katz J, Knio O (1999) The flow structure in the near field of jets and its effect on cavitation inception. J Fluid Mech 398:1–43

    Google Scholar 

  • Gopalan S, Katz J, Liu HL (2002) Effect of gap size on tip leakage cavitation inception, associated noise and flow structure. J Fluid Eng 124(4):994–1004

    Google Scholar 

  • Green SL (1995) Fluid vortices. Kluwer, Dordrecht, The Netherlands

    Google Scholar 

  • Iyer CO, Ceccio SL (2002) The influence of developed cavitation on the flow of a turbulent shear layer. Phys Fluids 14(10):3414–3431

    Google Scholar 

  • Judge C, Oweis GF, Ceccio SL, Jessup S, Chesnakas C, Fry DJ (2001) PIV Measurements of a tip leakage vortex. In: Proceedings of the 4th international symposium on cavitation (CAV 2001), Pasadena, California, June 2001

  • Katz J, O’Hern TJ (1986) Cavitation in large scale shear flow. Trans ASME J Fluids Eng 108:373–376

    Google Scholar 

  • Lakshminarayana B (1996) Fluid dynamics and heat transfer of turbomachinery. Wiley, New York

    Google Scholar 

  • O’Hern TJ (1990) An experimental investigation of turbulent shear flow cavitation. J Fluid Mech 215:365–391

    Google Scholar 

  • Ortega JM, Bristol RL, Savas Ö (2003) Experimental study of the instability of unequal-strength counter-rotating vortex pairs. J Fluid Mech 474:35–84

    Google Scholar 

  • Oweis GF, Choi J, Ceccio SL (2004) Dynamics and noise emissions of laser induced bubbles in a vortical flow field. J Acoust Soc Am, 115(3):1049–1058

    Google Scholar 

  • Oweis GF, Jessup SD, Chesnakas CJ, Fry DJ, Ceccio SL (2005a) Development of a tip-leakage flow. Part 1: the flow over a range of Reynolds numbers. ASME J Fluids Eng (accepted)

    Google Scholar 

  • Oweis GF, Jessup SD, Chesnakas CJ, Fry DJ, Ceccio SL (2005b) Development of a tip-leakage flow. Part 2: comparison between the ducted and unducted rotor. ASME J Fluid Eng (accepted)

    Google Scholar 

  • Oweis GF, van der Hout IE, Iyer C, Tryggvason G, Ceccio SL (2005c) Capture and inception of bubbles near line vortices. Phys Fluids 17(2):Art.no. 022105

    Google Scholar 

  • Raffel M, Willert C, Kompenhans J (1998) Particle image velocimetry. A practical guide. Springer, Berlin Heidelberg New York

    Google Scholar 

  • Ran B, Katz J (1994) Pressure fluctuations and their effect on cavitation inception within water jets. J Fluid Mech 262:223–263

    CAS  Google Scholar 

  • Spalart PR (1998) Airplane trailing vortices. Annu Rev Fluid Mech 30:107–138

    Google Scholar 

  • Straka WA, Farrel KJ (1992) The effect of spatial wandering on the experimental laser velocimetry measurements of the end-wall vortices in an axial flow pump. Exp Fluids 13:163–170

    Google Scholar 

  • Uzol O, Chow YC, Katz J, Meneveau C (2002) Experimental investigation of unsteady flow field within a two-stage axial turbomachine using particle image velocimetry. ASME J Turbomachinery 124:542–552

    Google Scholar 

  • von Karman Institute for Fluid Dynamics (1997) Lecture series von Karman Institute for Fluid Dynamics, vol. 1. Rhode Saint Genèse, Belgium, ISSN 0377-8312

  • Wernet MP (2000) Development of digital particle image velocimetry for use in turbomachinery. Exp Fluids 28:97–115

    Google Scholar 

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Acknowledgements

The authors acknowledge the contributions of Dr. Stuart Jessup, Dr. Christopher Chesnakas, and Dr. David Fry during the design and implementation of the experiment and would like to thank them for their permission to use the images in Figs. 1 and 2. This work was funded by the Office of Naval Research under grant number N00014-99-1-0307, with Dr. Ki-Han Kim as the technical monitor.

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Correspondence to Ghanem F. Oweis.

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Oweis, G.F., Ceccio, S.L. Instantaneous and time-averaged flow fields of multiple vortices in the tip region of a ducted propulsor. Exp Fluids 38, 615–636 (2005). https://doi.org/10.1007/s00348-005-0938-z

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  • DOI: https://doi.org/10.1007/s00348-005-0938-z

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