Title :
A simple three component velocity measurement method using a rotated split-film sensor
Author :
Miller, L.S. ; Yano, K.
Author_Institution :
Dept. of Aerosp. Eng., Wichita State Univ., KS, USA
Abstract :
A rotated split-film anemometry method which can be used to obtain three-component average flow velocities is reviewed and evaluated. The related theory, apparatus, calibration procedure, and results of the new technique are discussed. The new technique utilizes a single split-film probe in combination with a mechanical rotating probe, holder. The basic procedure is to make a plane or two-component velocity measurement with the probe in one orientation and then to rotate the probe 90° and make another measurement. The two pairs of velocity and flow angle data, are correlated, for yawed flow effects, and resolved to identify three (steady-flow) speed and direction components. Measurements in an axisymmetric jet at various flow speeds and angles indicate that the method has, under most circumstances, errors of about 5%. Slightly greater errors were encountered at extreme test flow speeds and at large sensor yaw and pitch angles
Keywords :
anemometry; flow measurement; jets; velocity measurement; axisymmetric jet; calibration; flow angle data; mechanical rotating probe, holder; rotated split-film sensor; three component velocity measurement; three-component average flow velocities; yawed flow effects; Calibration; Costs; Error correction; Fluid flow measurement; Linear discriminant analysis; Probes; Rotation measurement; Temperature sensors; Thermal sensors; Velocity measurement;
Conference_Titel :
Instrumentation in Aerospace Simulation Facilities, 1991. ICIASF '91 Record., International Congress on
Conference_Location :
Rockville, MD
DOI :
10.1109/ICIASF.1991.186250