This work was supported by the project “Development of Advanced Wings Solutions (DAWS)” funded by Innovate UK (46357). This work also received financial support from the program grant “Digital twins for improved dynamic design” funded by EPSRC (EP/R006768/1), and support from the Centre for Doctoral Training in Quantification and Management of Risk and Uncertainty in Complex Systems and Environments which is jointly funded by EPSRC and ESRC (EP/L015927/1). To report corrections or suggest improvements, please contact.