Hostname: page-component-cb9f654ff-65tv2 Total loading time: 0 Render date: 2025-08-22T22:16:18.051Z Has data issue: false hasContentIssue false
  • English
  • Français

Preliminary results from a particle imagevelocimetry study of blade–vortexinteraction

Published online by Cambridge University Press:  04 July 2016

M. B. Horner ,
J. N. Stewart ,
R. A. McD. Galbraith ,
I. Grant ,
F. N. Coton  and
G. H. Smith
Get access Rights & Permissions [Opens in a new window]

Summary

The results of a blade-vortex interaction (BVI) studyincorporating particle image velocimetry (PIV) arepresented. Test cases encompass a variety ofintersection geometries, including head-on parallelinteractions. Results provide quantified flowvisualisation images of the flows generated near theblade tip and inboard during interactions. PIVresults are examined in the light of understandinggained from previous pressure measurements made fromthe same BVI facility. Both the difficulties and theadvantages of utilising the PIV technique in thisapplication are discussed.

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 99 , Issue 983 , March 1995 , pp. 91 - 98
Copyright
Copyright © Royal Aeronautical Society 1995 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

Article purchase

Temporarily unavailable

Footnotes

†

Now at the National Wind Technology Center,National Renewable Energies Laboratory, Colorado,USA

† †

Now at Imperial College of Science, Technologyand Medicine, London

*

University of Glasgow, Glasgow, Scotland

⁺

Heriot-Watt University, Edinburgh, Scotland

References

1. Scheiman, J. and Ludi, L.H. Qualitative evaluation of effect of helicopter rotor-blade tip vortex on blade airloads, NASA TN D-1637, May 1963.Google Scholar
2. Brotherhood, P. and Riley, M.J. Flight experiments on aerodynamic features affecting helicopter blade design, Vertica, 1978, 2, pp 27–42.Google Scholar
3. Schmitz, F.H., Boxwell, D.A., Lewy, S. and Dahan, C. Model-to full-scale comparisons of helicopter blade-vortex interaction noise, 38th Annual National Forum of the American Helicopter Society, Anaheim, California, May 1978.Google Scholar
4. Surendraiah, M. An MS Thesis Experimental Study of Rotor Blade-Vortex Interaction, The Pennsylvania State University, December 1969.Google Scholar
5. Padakannaya, R. Experimental study of rotor unsteady airloads due to blade vortex interaction, NASA CR-1909, November 1971.Google Scholar
6. Caradonna, F.X., Laub, G.H. and Tung, C. An experimental study of rotor-vortex interaction, NASA TM-86005, November 1984.Google Scholar
7. Caradonna, F.X., Lautenschlager, J.L. and Silva, M.J. An experimental study of rotor-vortex interactions, AIAA Paper 88–0045, AIAA 26th Aerospace Sciences Meeting, Reno, Nevada, January 1988.Google Scholar
8. Caradonna, F.X., Strawn, R.C., and Bridgeman, J.O. An experimental and computational study of rotor-vortex interactions, 14th European Rotorcraft and Powered Lift Aircraft Forum, Milano, Italy, September 1988.Google Scholar
9. Kokkalis, A. and Galbraith, R.A.McD. Description of, and pre liminary results from, a new blade-vortex interaction test facility, 12th European Rotorcraft and Powered Lift Aircraft Forum, Garmisch-Partenkirchen, Federal Republic of Germany, September 1986.Google Scholar
10. Kokkalis, A. and Galbraith, R.A.McD. Results from the Glasgow University Blade-Vortex Interaction Facility, 13th European Rotor craft and Powered Lift Aircraft Forum, Aries, France, September 1987.Google Scholar
11. Saliveros, E. and Galbraith, R. A. McD. Collected Data From Blade Vortex Interaction Tests Using a Single Blade, Non-Lifting Rotor; Vol I: 94% Span, G.U. Aero Report 9007, Glasgow University, March 1990.Google Scholar
12. Saliveros, E. and Galbraith, R. A. McD. Collected Data From Blade Vortex Interaction Tests Using a Single Blade, Non-Lifting Rotor; Vol II: 86% Span, G.U. Aero Report 9008, Glasgow University, March 1990.Google Scholar
13. Saliveros, E. and Galbraith, R. A. McD. Collected Data From Blade Vortex Interaction Tests Using a Single Blade, Non-Lifting Rotor; Vol III: 78% Span, G.U. Aero Report 9009, Glasgow University, March 1990.Google Scholar
14. Saliveros, E. and Galbraith, R. A. McD. Collected Data From Blade Vortex Interaction Tests Using a Single Blade, Non-Lifting Rotor; Vol IV: 70% Span, G.U. Aero Report 9010, Glasgow University, March 1990.Google Scholar
15. Saliveros, E. and Galbraith, R. A. McD. Collected Data From Blade Vortex Interaction Tests Using a Single Blade, Non-Lifting Rotor; Vol V: 62% Span, G.U. Aero Report 9011, Glasgow University, March 1990.Google Scholar
16. Horner, M.H., Saliveros, E., Kokkalis, A., and Galbraith, R.A.McD. Results from a set of low speed blade-vortex interaction experiments, J of Experiments in Fluids, May 1993,14, pp 341–352. 14.Google Scholar
17. Horner, M.H., Saliveros, E., and Galbraith, R.A.McD. An exper imental investigation of the oblique blade-vortex interaction, 17th European Rotorcraft and Powered Lift Aircraft Forum, Berlin, Germany, September 1991.Google Scholar
18. Horner, M.H., Saliveros, E., and Galbraith, R.A.McD. An examination of vortex convection effects during blade-vortex interaction, AHS/RAeS Technical Specialists Meeting on Rotorcraft Acoustics and Rotor Fluid Dynamics, Philadelphia, USA, October 1991.Google Scholar
19. Seath, D.D. Vortex-airfoil interaction tests, 2nd Atmospheric Flight Mechanics Conference, Palo Alto and Moffett Field, California, September 1972.Google Scholar
20. Seath, D.D., Kim, J.M. and Wilson, D.R. An investigation of the parallel blade-vortex interaction in low-speed wind tunnel, AIAA Paper 87–1345, AIAA 19th Fluid Dynamics, Plasma Dynamics and Lasers Conference, Honolulu, Hawaii, June 1987.Google Scholar
21. Ham, N.D. Some preliminary results from an investigation of blade-vortex interactions, J of the American Helicopter Society, April 1974,19, pp 45–48.Google Scholar
22. Hum, N.D. Some conclusions from an investigation on blade-vortex interaction, J of the American Helicopter Society, October 1975, 20, pp 26–31.Google Scholar
23. Booth, E.R. Jr and Yu, .C. Two-dimensional blade-vortex flow visualisation investigation, AIAA J, September 1986, 24, (9).Google Scholar
24. Booth, E.R. Jr Surface pressure measurement during low speed two-dimensional blade vortex interaction, AIAA Paper 86-1856, AIAA 10th Aeroacoustics Conference, Seattle, Washington, July 1986.Google Scholar
25. Meier, G.E.A. and Timm, R. Unsteady vortex airfoil interaction, AGARD CP-386, May 1985.Google Scholar
26. Straus, J., Renzoni, O. and Mayle, R.E. Airfoil pressure measurements during a blade-vortex interaction and a comparison with theory, AIAA Paper 88–0669, AIAA 26th Aerospace Sciences Meeting, Reno, Nevada, January 1988.Google Scholar
27. Huyer, S. A., and Luttges, M. W. Unsteady flow interactions between the wake of an oscillating airfoil and a stationary trailing airfoil, AIAA Paper 88–2581, AIAA 6th Applied Aerodynamics Conference, Williamsburg, Virginia, June 1988.Google Scholar
28. Ziada, S. and Rockwell, D. Vortex-leading edge interaction, J of Fluid Mechs, 1982, 118, pp 79–107.Google Scholar
29. Walker, J. Dynamic stall wake interaction with a trailing aerofoil, AIAA Paper 87–0239, AIAA 25th Aerospace Sciences Meeting, Reno, Nevada, January 1987.Google Scholar
30. Sears, W.R. Aerodynamics, noise and the sonic boom, AIAA J, April 1969, 7, (4).Google Scholar
31. Panaras, A. Numerical modelling of the vortex-airfoil interaction, AIAA J, January 1987, 25, (1).Google Scholar
32. Lee, D.J. and Smith, C.A. Distortion of vortex core during blade/Vortex interaction, AIAA Paper 87–1243, AIAA 19th. Fluid. Dynamics, Plasma Dynamics & Lasers Conference Honolulu, Hawaii, June 1987.Google Scholar
33. Jones, H.E., and Caradonna, F.X. Full potential modelling of blade-vortex interactions, Vertica, 1988, 12, (1/2), pp 129–145.Google Scholar