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Investigation on flight load calibration of aircraft composite wing base on strain gauge measurement
Publikováno v:
Theoretical and Applied Mechanics Letters, Vol 14, Iss 5, Pp 100540- (2024)
A computational and test method for calibrating the flight loads carried by aircraft wings is proposed. The wing load is measured in real-time based on the resistance and fiber Bragg grating strain gauges. The linear stepwise regression method is use
Externí odkaz:
https://doaj.org/article/ead009c06c8b469b8828d78610e9c6c1
