This chapter describes the development of load monitoring systems integrated in the demonstrator of a smart wing structure. A monitoring system has been designed and installed on composite spars, with the aim of mapping the load conditions along the axes of such...
CITATION STYLE
Airoldi, A., Sala, G., Evenblij, R., Koimtzoglou, C., Loutas, T., Carossa, G. M., … Kanakis, T. (2016). Load Monitoring by Means of Optical Fibres and Strain Gages. In Smart Intelligent Aircraft Structures (SARISTU) (pp. 433–469). Springer International Publishing. https://doi.org/10.1007/978-3-319-22413-8_20
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