National Center for Atmospheric Research
EOL Integrated Surface Flux Facility

NCAR ISFF Sonic Anemometer Tilt Correction

Tilt of a sonic anemometer from true vertical can introduce errors in the measured sensible heat and momentum fluxes. The tilt error in u* or in a scalar flux is on the order of 5% per degree of tilt in the vertical plane aligned with the mean wind direction. Consequently, it is often necessary to rotate the coordinates of three-dimensional sonic wind data to correct for this tilt. NCAR estimates the sonic tilt angles from the archived wind data using the planar fit technique described in Wilczak, Oncley, and Stage, 2001, `Sonic anemometer tilt correction algorithms', Boundary Layer Meteor., 99, pp. 127-150. Briefly, this technique assumes that the time-averaged wind field is confined to a plane surface, nominally parallel to the ground. It is assumed that the fluxes of interest are those normal to this wind-field plane and thus the vertical velocity axis is re-oriented normal to that plane. The orientation of the wind-field plane relative to the measurement axes of the sonic anemometer is determined by a least-squares fit of the wind data to the equation

w = a + bu + cv

where u, v, w are the 5-minute-averaged horizontal and vertical wind components measured by the sonic anemometer. The fitted coefficients correspond to

vertical velocity offset = a

sonic lean angle = atan((b2 + c2)½)

azimuth of sonic lean (relative to u axis) = atan(c/b)

Confidence in the fit to this model requires data with as wide a range of wind directions as possible; in practice, 90° or greater. Thus confidence can best be achieved with data extending over many hours or days. If the data are available, this requirement is acceptable because the sonic tilt angles are expected to be unchanged unless the sonic anemometer is moved (or the surrounding surface itself changes!). Thus the tilt angles are calculated for periods delimited by known physical changes in the sonic orientation, e.g. re-leveling the mast or swapping the sonic anemometer.


Last modified: Wednesday, 30-Oct-2002
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This page was prepared by Tom Horst, NCAR ATD Research Technology Facility