27 November 1996 Application of the Hollow-Core Optical Sensor to measurement of static structural bending
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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.
© (1996) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Richard D. Teichgraeber, Richard D. Teichgraeber, Curtis L. Fischer, Curtis L. Fischer, Douglas S. Abernathy, Douglas S. Abernathy, Sandra Berning, Sandra Berning, } "Application of the Hollow-Core Optical Sensor to measurement of static structural bending", Proc. SPIE 2838, Distributed and Multiplexed Fiber Optic Sensors VI, (27 November 1996); doi: 10.1117/12.259795; https://doi.org/10.1117/12.259795
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