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Two-Axis Direct Fluid Shear Stress Sensor for Aerodynamic ApplicationsThis miniature or micro-sized semiconductor sensor design provides direct, nonintrusive measurement of skin friction or wall shear stress in fluid flow situations in a two-axis configuration. The sensor is fabricated by microelectromechanical system (MEMS) technology, enabling small size and multiple, low-cost reproductions. The sensors may be fabricated by bonding a sensing element wafer to a fluid-coupling element wafer. Using this layered machine structure provides a truly three-dimensional device.
Document ID
20110011951
Acquisition Source
Goddard Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Bajikar, Sateesh S.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Scott, Michael A.
(NASA Langley Research Center Hampton, VA, United States)
Adcock, Edward E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
April 1, 2011
Publication Information
Publication: NASA Tech Briefs, April 2011
Subject Category
Instrumentation And Photography
Report/Patent Number
GSC-15431-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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