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Proceedings Paper

Application of the Hollow-Core Optical Sensor to measurement of static structural bending
Author(s): Richard D. Teichgraeber; Curtis L. Fischer; Douglas S. Abernathy; Sandra Berning
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Paper Abstract

An application of a linear fiberoptic sensor for detection and measurement of structural bending is described. Design, development and fabrication of the sensor is described, along with details of static bench testing and static structural bending tests of an actual aircraft wing. Knowledge of inflight aircraft surface flexure may be important for certain surveillance sensor and weapon delivery computational applications.

Paper Details

Date Published: 27 November 1996
PDF: 10 pages
Proc. SPIE 2838, Distributed and Multiplexed Fiber Optic Sensors VI, (27 November 1996); doi: 10.1117/12.259795
Show Author Affiliations
Richard D. Teichgraeber, Lockheed Martin Tactical Aircraft Systems (United States)
Curtis L. Fischer, Lockheed Martin Tactical Aircraft Systems (United States)
Douglas S. Abernathy, Lockheed Martin Tactical Aircraft Systems (United States)
Sandra Berning, Air Force Wright Lab. (United States)


Published in SPIE Proceedings Vol. 2838:
Distributed and Multiplexed Fiber Optic Sensors VI
Alan D. Kersey; John P. Dakin, Editor(s)

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