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{{UFR|front=UFR 1-02|description=UFR 1-02 Description|references=UFR 1-02 References|testcase=UFR 1-02 Test Case|evaluation=UFR 1-02 Evaluation|qualityreview=UFR 1-02 Quality Review|bestpractice=UFR 1-02 Best Practice Advice|relatedACs=UFR 1-02 Related ACs}}
{{UFR|front=UFR 1-02|description=UFR 1-02 Description|references=UFR 1-02 References|testcase=UFR 1-02 Test Case|evaluation=UFR 1-02 Evaluation|qualityreview=UFR 1-02 Quality Review|bestpractice=UFR 1-02 Best Practice Advice|relatedACs=UFR 1-02 Related ACs}}


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== References ==
== 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”, 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.
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
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.
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.
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.
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.
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
Wallin, S. and Girimaji, S.S, 2000, “Evolution of an isolated turbulent trailing vortex”, AIAA Journal, Vol. 38, No. 4. April 2000., 657 – 712


 


10. acknowledgement
=== Acknowledgement ===


All of the figures included in this UFR are published by kind permission of the American Institute of Aeronautics and Astronautics, as follows
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 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
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


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<font size="-2" color="#888888">© copyright ERCOFTAC 2004</font><br />
<font size="-2" color="#888888">© copyright ERCOFTAC 2004</font><br />
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Contributors: Michael Casey - Sulzer Innotec AG
Contributors: Michael Casey - Sulzer Innotec AG
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{{UFR|front=UFR 1-02|description=UFR 1-02 Description|references=UFR 1-02 References|testcase=UFR 1-02 Test Case|evaluation=UFR 1-02 Evaluation|qualityreview=UFR 1-02 Quality Review|bestpractice=UFR 1-02 Best Practice Advice|relatedACs=UFR 1-02 Related ACs}}
{{UFR|front=UFR 1-02|description=UFR 1-02 Description|references=UFR 1-02 References|testcase=UFR 1-02 Test Case|evaluation=UFR 1-02 Evaluation|qualityreview=UFR 1-02 Quality Review|bestpractice=UFR 1-02 Best Practice Advice|relatedACs=UFR 1-02 Related ACs}}
[[Category:Underlying Flow Regime]]

Latest revision as of 19:05, 11 February 2017

Front Page

Description

Test Case Studies

Evaluation

Best Practice Advice

References




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


Front Page

Description

Test Case Studies

Evaluation

Best Practice Advice

References

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