Abstract
Three-component particle image velocimetry measurements at moderate speeds and observation distances can now be accomplished on a routine basis. This article discusses the experiment performed on a 4 m-diameter model rotor in the 6-m×8-m open test section of the Large Low Speed Facility of the German–Dutch Wind Tunnels. More than half a terabyte of raw data were recorded at various positions on the advancing and retreating sides of the rotor in order to obtain detailed measurements of the trailing vortex in the frame of an international project. This paper addresses measuring techniques and possible sources of errors and presents a limited number of cases for the purpose of illustrating the solutions to numerous technical challenges relating to the acquisition and analysis of vortical flows.
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Abbreviations
- C T :
-
thrust coefficient (T/ρπΩ2 R 4)
- M :
-
magnification
- r c :
-
radius of vortex core (mm)
- R :
-
rotor radius (m)
- T :
-
thrust (N)
- u,v,w :
-
velocity components in x, y and z coordinates (m/s)
- (u,v,w)wt :
-
velocity components in wind tunnel coordinates (m/s)
- U max :
-
maximum in-plane velocity component (m/s)
- W max :
-
maximum out-of-plane velocity component (m/s)
- x,y,z :
-
particle image velocimetry (PIV) frame coordinates (m)
- (x,y,z)wt :
-
wind tunnel coordinates (m)
- Δt :
-
time delay (μs)
- ΔZ :
-
light sheet thickness (mm)
- ΔZ :
-
light sheet thickness (mm)
- Ω:
-
rotor rotation frequency (rad/s)
- ψ :
-
rotor azimuth angle during recording (deg) vortex age
- α :
-
rotor shaft angle (deg)
- ε x :
-
displacement measurement error
- μ :
-
advance ratio (V/ΩR)
- ρ :
-
air density (kg/m3)
- τ :
-
circulation (m2/s)
- ω z :
-
vorticity (s−1)
- AFDD:
-
Aeroflightdynamics Directorate
- BVI:
-
blade–vortex interaction
- DLR:
-
Deutches zentrum für Luft- und Raumfahrt
- DNW:
-
German–Dutch Wind tunnel
- HART:
-
HHC aeroacoustic rotor test
- LLF:
-
large low speed facility
- NASA:
-
National Aeronautics and Space Administration
- ONERA:
-
Office National d’Etudes e de Recherches Aerospatiales
- RANS:
-
Reynolds-averaged Navier–Stokes
- SPR:
-
stereo pattern recognition
- 3C-PIV:
-
three-component particle image velocimetry
References
Caradonna FX, Lautenschläger JL, Silva MJ (1988) An experimental study of rotor–vortex interaction. Aerospace Science Meeting, Reno, NV, Paper AIAA 88-0045
Ehrenfried K (2001) Processing calibration-grid images using the Hough transformation. Meas Sci Technol 13:975–984
Ehrenfried K, Meier GEA, Obermeier F (1991) Sound produced by vortex–airfoil interaction. 17th ERF, Berlin, Germany, Paper 63
Gauthier V, Riethmuller ML (1988) Application of PIDV to complex flows: measurements of the third component. Particle Image Displacement Velocimetry, Von Karman Institute for Fluid Mechanics, Rhode-Saint-Genese, Belgium, Paper VKI-LS 1988-06
Gaydon M, Raffel M, Willert C, Rosengarten M, Kompenhans J (1997) Hybrid stereoscopic particle image velocimetry. Exp Fluids 23:331–334
Grant I (1994) Selected papers on particle image velocimetry. SPIE Milestone Series. SPIE Optical Engineering Press, Bellingham, WA
Hart DP (1998) PIV error correction. In: Proceedings of the 9th International Symposium on Applications of laser technology to fluid mechanics, Lisbon, Portugal. Instituto Superior Técnico, Lisbon
Heineck JT, Yamauchi GK, Wadcock AJ, Lourenco LM, Abrego AI (2000) Application of three-component PIV to a hovering rotor wake. AHS 56th Annual Forum, Virginia Beach, VA, USA
Kähler C (2000) Multiplane stereo PIV—recording and evaluation methods. In: EUROMECH 411, Application of PIV to turbulence measurements, Rouen, France
Keane RD, Adrian RJ (1992) Theory of cross-correlation analysis of PIV image. Appl Sci Res 49:191–215
Leishman JG (1998) Measurements of the aperiodic wake of a hovering rotor. Exp Fluids 25:352–361
Leishman JG, Bagai A (1996) Challenges in understanding the vortex dynamics of helicopter rotor wakes. AIAA J 36:1130–1140
Martin PB, Pugliese GJ, Leishman JG (2001) High resolution trailing vortex measurements in the wake of a hovering rotor. AHS 57th Annual Forum, Washington, DC, USA
McAlister KW, Tung C, Heineck JT (2001) Forced diffusion of trailing vorticity from a hovering rotor. AHS 57th Annual Forum, Washington, DC, USA
McCroskey WJ (1995) Vortex wakes of rotorcraft. 33rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, Paper 95-0530
Murashige A, Tsuchihashi A, Tsujiuchi T, Yamakawa E (1997) Blade tip vortex measurement by PIV. 23rd ERF, Dresden, Germany, Paper 36
Raffel M, De Gregorio F, Pengel K, Willert C, Kähler C, Ehrenfried K, Kompenhans J (1998a) Instantaneous flow field measurements for propeller aircraft and rotorcarft research. In: Proceedings of the 9th International Symposium on Applications of laser technology to fluid mechanics, Lisbon, Paper 19.6. Instituto Superior Técnico, Lisbon
Raffel M, Willert C, Kompenhans J (1998b) Particle image velocimetry, a practical guide. Springer, Heidelberg Berlin New York
Schram C, Riethmuller ML (2001) Vortex ring evolution in an impulsively started jet using digital image particle velocimetry and continuous wavelet analysis. Meas Sci Technol 13:1413–1421
Splettstößer WR, Kube R, Wagner W, Seelhorst U, Boutier A, Micheli F, Mercker E (1995) Key results from a higher harmonic control aeroacoustic rotor test (HART) in the German–Dutch wind tunnel. 21st European Rotorcraft Forum, St Petersburg, Russia
Splettstößer WR, Schultz KJ, Boxwell DA, Schmitz FH (1984) Helicopter model rotor blade/vortex interaction impulsive noise; scalability and parametric variations. NASA TM 86007
Strawn RC, Oliker L, Biswas R (1996) New computational methods for the prediction and analysis of helicopter noise. 2nd AIAA/CEAS Aeroacoustics Conference, State College, PA, May 1996, USA
Vogt A, Baumann P, Gharib M, Kompenhans J (1996) Investigations of a wing tip vortex in air by means of DPIV. 19th AIAA Advanced Measurement and Ground Testing Technology, New Orleans, LA, Paper AIAA 96-2254
Yu Y (2002) The HART program: joint international rotor aeroacoustics test and analysis validation program. AHS International Technical Specialist Meeting, San Francisco, CA
Yu Y, Tung C, van der Wall B, Pausder H, Burley C, Brooks T, Beaumier P, Delrieux Y, Mercker E (2002) The HART-II test: rotor wakes and aeroacoustics with higher harmonic pitch control (HHC) inputs—the joint German/French/Dutch/US project. AHS 58th Annual Forum, Montreal, Canada
Acknowledgements
The authors would like to especially thank the engineers and technicians of DLR Braunschweig for their cooperation, as well as many others that took part in the measurements. We would also like to acknowledge C. Schram for his help and support in analyzing the vortex characteristics. We highly appreciate the productive and excellent partnership of the HART II community, who gave us the opportunity to perform these measurements.
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Raffel, M., Richard, H., Ehrenfried, K. et al. Recording and evaluation methods of PIV investigations on a helicopter rotor model. Exp Fluids 36, 146–156 (2004). https://doi.org/10.1007/s00348-003-0689-7
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DOI: https://doi.org/10.1007/s00348-003-0689-7