| タイトル | Thermal effects on fiber optic strain sensors embedded in graphite-epoxy composites |
| 著者（英） | Dehart, D. W.; Heyman, J. S.; Holben, M. S., Jr.; Rogowski, R. S.; Margulies, Susan |
| 著者所属（英） | Air Force Astronautics Lab.; NASA Langley Research Center; AS&M, Inc. |
| 発行日 | 1990-01-01 |
| 言語 | eng |
| 内容記述 | Smart structures deployed in low earth orbit will be exposed to a hostile environment which will include temperature extremes during each orbit as the platform moves from the day to the night side. The stresses due to thermal cycling may compromise the performance of embedded fiber optic strain sensors because of differential thermal expansion of the fiber and the composite material. The effects of elevated temperature and thermal cycling on the performance of a fiber optic strain sensor embedded in a graphite-epoxy tube have been investigated for temperatures from 65 to 220 F. The results indicate that the fiber optic strain sensor measurements correlate well with conventional resistance strain gages attached to the tube. |
| NASA分類 | INSTRUMENTATION AND PHOTOGRAPHY |
| レポートNO | 90A32894 |
| 権利 | Copyright |
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