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Direct Shear Stress Sensor Characterization in the NASA 13” Flow FacilityThis paper describes the testing of a commercially available shear stress sensor with emphasis on an examination of the output data and how variations in the output characteristics impacted the data analysis. The sensor itself is 0.625” in diameter with a length of 2” with a 0.375” diameter floating element and the sensor and housing constructed of stainless steel and aluminum. Shear stress was measured/calculated real time and compared to the output of the shear stress sensor. The range of testing was up to 15 Pa compared to the maximum calibrated range of 300 Pa for the sensor. The resultant sensitives of this device are within the expected range.
Document ID
20205002731
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Michael A Scott
(Langley Research Center Hampton, Virginia, United States)
Edward E Adcock
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 26, 2020
Subject Category
Instrumentation And Photography
Meeting Information
Meeting: AIAA SciTech Forum and Exposition
Location: Nashville, TN
Country: US
Start Date: January 11, 2021
End Date: January 15, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 109492.02.07.05.06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Shear Stress
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