UFR 1-02 References: Difference between revisions
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Blade tip and tip clearance vortex flow
Underlying Flow Regime 1-02 © copyright ERCOFTAC 2004
References
Chow, J., Zilliac, G., Bradshaw, P., 1997, “Turbulence measurements in the near field of a wing-tip vortex”, NASA TECH Memo110418.
Chow, J., Zilliac, G., Bradshaw, P., 1997, “Turbulence measurements in the near field of a wing-tip vortex” AIAA Journal Vol.35, page 1561.
Dacles-Mariani, J., Zilliac, G., Chow, J., Bradshaw, P., 1995, “Numerical/Experimental study of a wing-tip vortex in the near field” AIAA Journal Vol.33, No 9, page 1561
Hsiao C-T and Pauley L.L., 1998, “Numerical study of the steady state tip vortex flow over a finite-span hydrofoil” Trans ASME Journal of Fluids Engineering, Vol 120,, No 2 June, pp345-353.
Kang, S., and Hirsch, C., 1993, “Experimental Study on the Three-Dimensional Flow within a Compressor Cascade with Tip Clearance: Part I-Velocity and Pressure Fields, and Part II-The Tip Leakage Vortex,” ASME J. Turbomach., 115, pp. 435-443.
Rizzetta, D. P, 1996, “Numerical investigations of supersonic wing-tip vortices”, AIAA Journal, Vol. 34, No. 6, April, 1167 – 1173.
Snyder, D., and Spall, R., 2000, “Numerical investigation into multiple vortex structures formed over flat end-cap wings”, AIAA Journal, Vol 38, No. 8, August, pp1486- 1489.
Wallin, S. and Girimaji, S.S, 2000, “Evolution of an isolated turbulent trailing vortex”, AIAA Journal, Vol. 38, No. 4. April 2000., 657 – 712
Acknowledgement
All of the figures included in this UFR are published by kind permission of the American Institute of Aeronautics and Astronautics, as follows
Figures 1 and 2 are figures are from Chow, J., Zilliac, G., Bradshaw, P., 1997, “Turbulence measurements in the near field of a wing-tip vortex” AIAA Journal Vol.35, page 1561.
Figures 3, 4 and 5 are from Dacles-Mariani, J., Zilliac, G., Chow, J., Bradshaw, P., 1995, “Numerical/Experimental study of a wing-tip vortex in the near field” AIAA Journal Vol.33, No 9, page 1561
© copyright ERCOFTAC 2004
Contributors: Michael Casey - Sulzer Innotec AG