NASA NTRS · 19880014375
Crossflow vorticity sensor
Abstract
A crossflow vorticity sensor for the detection of crossflow vorticity characteristics is described. The sensor is comprised of crossflow sensors which are noninvasively adhered to a swept wing laminar surface either singularly, in multi-element strips, in polar patterns, or in orthogonal patterns. These crossflow sensors are comprised of hot-film sensor elements which operate as a constant temperature anemometer circuit to detect heat transfer rate changes. Accordingly, crossflow vorticity characteristics are determined via cross-correlation. In addition, the crossflow sensors have a thickness which does not exceed a maximum value h in order to avoid contamination of downstream crossflow sensors.
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Holmes, Bruce J., Carraway, Debra L., Holmes, Harlan K., Moore, Thomas C.. 1988-03-01. Crossflow vorticity sensor. https://ntrs.nasa.gov/citations/19880014375
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