Health Monitoring of the Aircraft Structure during a Full Scale Fatigue Test with Use of an Active Piezoelectric Sensor Network

Publisher: Trans Tech Publications

E-ISSN: 1662-9779|2015|220|328-332

ISSN: 1012-0394

Source: Solid State Phenomena, Vol.2015, Iss.220, 2015-01, pp. : 328-6

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

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Abstract