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An arrayed hot-film sensor for detection of laminar boundary-layer flow disturbance spatial characteristicsAn arrayed hot-film sensor has been developed for use in laminar boundary-layer research for the detection of crossflow or Goertler vortices. This sensor has been developed to detect spatial variations in heat transfer which are characteristic of crossflow or Goertler vortices. The sensor is ultimately intended for flight research applications. This paper describes the sensor, its priciples of operation, signal analysis techniques, and experimental results illustrating the spatial detection capabilities of this specialized hot-film device. Discretely placed spheres placed in the boundary layer created alternating regions of undisturbed and disturbed laminar flow over a prototype sensor. Flow visualization results were correlated with the sensor output to demonstrate the ability of the sensor to determine the spatial boundaries of localized disturbances in laminar flow. This work represents the initial steps toward the validation and calibration of an arrayed hot-film sensor for the detection of crossflow or Goertler vorticity wavelength and/or wave frequency.
Document ID
19880066604
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wusk, M. S.
(NASA Langley Research Center Hampton, VA, United States)
Carraway, D. L.
(NASA Langley Research Center Hampton, VA, United States)
Holmes, B. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
September 1, 1988
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA PAPER 88-4677
Report Number: AIAA PAPER 88-4677
Accession Number
88A53831
Distribution Limits
Public
Copyright
Other

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