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Crossflow vorticity sensorA 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.
Document ID
19880014375
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Holmes, Bruce J.
(NASA Langley Research Center Hampton, VA, United States)
Carraway, Debra L.
(Old Dominion Univ. Hampton, Va., United States)
Holmes, Harlan K.
(NASA Langley Research Center Hampton, VA, United States)
Moore, Thomas C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
March 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-003676
Patent Number: NASA-CASE-LAR-13436-1-CU
Patent Number: US-PATENT-4,727,751
Accession Number
88N23759
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LAR-13436-1-CU|US-PATENT-4,727,751
Patent Application
US-PATENT-APPL-SN-003676
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