NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A Two-Axis Direct Fluid Shear Stress SensorThis innovation is a miniature or micro sized semiconductor sensor design that provides two axis direct non-intrusive measurement of skin friction or wall shear stress in fluid flow. The sensor is fabricated by micro-electro-mechanical system (MEMS) technology, enabling small size and low cost reproductions. The sensors have been fabricated by utilizing MEMS fabrication processes to bond a sensing element wafer to a fluid coupling wafer. This layering technique provides for an out of plane dimension that is on the same order of length as the inplane dimensions. The sensor design has the following characteristics: a shear force collecting plate with dimensions that can be tailored to various application specific requirements such as spatial resolution, temporal resolution and shear force range and resolution. This plate is located coplanar to both the sensor body and flow boundary, and is connected to a dual axis gimbal structure by a connecting column or lever arm. The dual axis gimbal structure has torsional hinges with embedded piezoresistive torsional strain gauges which provide a voltage output that is correlated to the applied shear stress (and excitation current) on force collection plate that is located on the flow boundary surface (hence the transduction method). This combination of design elements create a force concentration and resolution structure that enables the generation of a large stress on the strain gauge from the small shear stress on the flow boundary wall. This design as well as the use of back side electrical contacts establishes a non-intrusive method to quantitatively measure the shear force vector on aerodynamic bodies.
Document ID
20100022049
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Adcock, Edward E.
(NASA Langley Research Center Hampton, VA, United States)
Scott, Michael A.
(NASA Langley Research Center Hampton, VA, United States)
Bajikar, Sateesh S.
(QSS Group, Inc. Greenbelt, MD, United States)
Date Acquired
August 24, 2013
Publication Date
May 1, 2010
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
L-19878
NASA/TM-2010-216696
NF1676L-10712
Report Number: L-19878
Report Number: NASA/TM-2010-216696
Report Number: NF1676L-10712
Funding Number(s)
WBS: WBS 698259.02.07.07.02.01
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available