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Flexible deflection measurements using the SansEC smart sensor

Menon, Alok N.
Whitford, Jonathan
Kostogorova-Beller, Yulia
Steck, James E.
Chakravarthy, Animesh
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2017-01-05
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Conference paper
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Optical sensor,Frequency response,Data analysis,Resonance frequencies,Aircraft wings,National Aeronautics and Space Administration,NASA,Electromotive forces,Network analyzer,Permittivity,Flight control system
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Alok Menon, Jonathan Whitford, Yulia Kostogorova-Beller, James E. Steck and Animesh Chakravarthy. "Flexible Deflection Measurements using the SansEC Smart Sensor," AIAA 2017-1586. 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. January 2017. https://doi.org/10.2514/6.2017-1586
Abstract
This paper investigates the use of the SansEC smart sensing technology towards mea-surement of bending and torsional deflections on a flexible plate. It is demonstrated that bending and torsional deflections result in changes in the frequency response of the SansECsensor. An experimental setup comprising of SansEC sensors mounted on a flexible plateis constructed, and this model is subjected to dynamic bending deflections and static tor-sional deflections, in separate tests. Frequency measurements of the SansEC sensor arerecorded, and a post-experimental data analysis is conducted. These results demonstrate astrong correlation between the plate deflections and the frequency response of the sensor,and demonstrate significant promise for use of the SansEC sensor towards measurement ofwing deflections in morphing aircraft applications.
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Presented at the 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 9 - 13 January 2017, Grapevine, Texas
AIAA 2017-1586 Session: Special Session: Adaptive Aeroelastic Wing Shaping Control I
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American Institute of Aeronautics and Astronautics
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Proceedings of the 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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