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9 July 1999 Fiber optic sensors for health monitoring of morphing aircraft
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Abstract
Fiber optic sensors are being developed for health monitoring of future aircraft. Aircraft health monitoring involves the use of strain, temperature, vibration and chemical sensors. These sensors will measure load and vibration signatures that will be used to infer structural integrity. Since the aircraft morphing program assumes that future aircraft will be aerodynamically reconfigurable there is also a requirement for pressure, flow and shape sensors. In some cases a single fiber may be used for measuring several different parameters.
© (1999) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Timothy L. Brown, Karen H. Wood, Brooks A. Childers, Roberto J. Cano, Brian J. Jensen, and Robert S. Rogowski "Fiber optic sensors for health monitoring of morphing aircraft", Proc. SPIE 3674, Smart Structures and Materials 1999: Industrial and Commercial Applications of Smart Structures Technologies, (9 July 1999); https://doi.org/10.1117/12.351590
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