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Shear Stress Sensing with Elastic Microfence StructuresIn this work, elastic microfences were generated for the purpose of measuring shear forces acting on a wind tunnel model. The microfences were fabricated in a two part process involving laser ablation patterning to generate a template in a polymer film followed by soft lithography with a two-part silicone. Incorporation of a fluorescent dye was demonstrated as a method to enhance contrast between the sensing elements and the substrate. Sensing elements consisted of multiple microfences prepared at different orientations to enable determination of both shear force and directionality. Microfence arrays were integrated into an optical microscope with sub-micrometer resolution. Initial experiments were conducted on a flat plate wind tunnel model. Both image stabilization algorithms and digital image correlation were utilized to determine the amount of fence deflection as a result of airflow. Initial free jet experiments indicated that the microfences could be readily displaced and this displacement was recorded through the microscope.
Document ID
20160005995
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Cisotto, Alexxandra
(NASA MUREP Scholar Hampton, VA, United States)
Palmieri, Frank L.
(NASA Langley Research Center Hampton, VA, United States)
Saini, Aditya
(North Carolina State Univ. Raleigh, NC, United States)
Lin, Yi
(National Inst. of Aerospace Hampton, VA, United States)
Thurman, Christopher S
(NASA Langley Research Center Hampton, VA, United States)
Kim, Jinwook
(North Carolina State Univ. Raleigh, NC, United States)
Kim, Taeyang
(North Carolina State Univ. Raleigh, NC, United States)
Connell, John W.
(NASA Langley Research Center Hampton, VA, United States)
Zhu, Yong
(North Carolina State Univ. Raleigh, NC, United States)
Gopalarathnam, Ashok
(North Carolina State Univ. Raleigh, NC, United States)
Jiang, Xiaoning
(North Carolina State Univ. Raleigh, NC, United States)
Wohl, Christopher J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
May 10, 2016
Publication Date
June 22, 2015
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-19956
Report Number: NF1676L-19956
Meeting Information
Meeting: AIAA Aviation 2015 Aerodynamic Measurement Technology and Ground Testing Conference
Location: Dallas, TX
Country: United States
Start Date: June 22, 2015
End Date: June 25, 2015
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 533127.02.93.07.14.34
Distribution Limits
Public
Copyright
Public Use Permitted.
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