Cover
Vol. 12 No. 1 (2012)

Published: July 31, 2012

Pages: 103-111

Original Article

Design and Calibration of Five- Holed Conical Probe for Fluid Velocity Measurements in Three Dimensions

Abstract

The performance of a five-holed conical probe ( which has a conical head with four holes symmetrically placed on the cone surface and one at the truncated tip) for the measurements of fluid velocity in three dimensional incompressible flow was investigated in air in an open circuit subsonic wind tunnel . The air velocity ranged from 15 – 45 m/s and the Reynolds number ranged from 40000 to 100000 based on the cone base diameter. The methods of calibration and use of the probe are given where the measurements of one angle and three pressures are sufficient to give the three components of velocity, static and total pressure. The conical head probe is easier to manufacture than the spherical head probe and has the advantage of having clear fluid separation points at the cone base whereas the fluid separation on the spherical probe is not well defined and depends on the Reynolds number.

References

  1. Pope A. and Goin, K.L., "High Speed Wind Tunnel Testing", Florida, Robert E Kreiger Publishing Company, 1978.
  2. Porro, A.R. and Ernst, M.A., "Apparatus for Measuring Ambient Pressure Within a Gaseous Flow Field", U.S. Patent Number 5,756,892, 1998.
  3. Shepherd, I.C., "A Four Hole Pressure Probe for Fluid Flow Measurements in Three Dimensions", ASME Journal of Fluids Engineering, Vol. 103, pp. 590–594, 1981.
  4. Dominy, R.G. and Hodson, H.P., "An Investigation of Factors Influencing the Calibration of 5-hole Cone and Pyramid Probes", ASME Journal of Turbomachinery, Vol. 115, pp. 513-519, July 1993.
  5. Chanson, H., "Measuring air-water interface area in supercritical open channel flow", Water Research, IAWPRC, 31(6), pp. 1414–1420, 1997.
  6. Bachalo, W. D., "Experimental methods in multiphase flows", Int. J. Multiphase Flow, 20, Suppl., pp. 261–295, 1994.
  7. Babinsky, H., Kuschel, U., Hodson, H.P., Moore, D.F., and Welland, M.E., "The Aerodynamic Design and Use of Multi-Sensor Pressure Probes for MEMS Applications", Turbomachines, Florence, Sep 28-29, 2000.
  8. Naughton, J.W., Cattafesta III, L.N., and Settles, G.S., "A Miniature, Fast-Response 5-Hole Probe for Supersonic Flowfield Measurement", AIAA–92–0266, 1992.
  9. University of Cambridge, Whittle Laboratory, "Pressure Probes", [Online]. Available: http://www.g.eng.cam.ac.uk/whittle/current-research/hph/pressureprobes/pressure-probes.html
  10. Corey Ippolito, "Wind Tunnel Calibration of the Exploration Aerial Vehicle (EAV) Five-Hole Pitot Probe", NASA Ames Research Center, Moffett Field, CA, August 8, 2006.