@inproceedings{91d9570086784165bb2ada1b29dc7072,
title = "The influence of morphing process on the aeroelastic characteristics of a folding wing",
abstract = "In the present study, a two-segment folding wing model is used to investigate the influence of morphing process on the aeroelastic characteristics. The structure model is formulated by the Lagrange equations, and the aerodynamic model based on the Doublet Lattice method is formulated by the Kriging agent model technique. The aeroelastic response of the two-segment folding wing during the morphing process is simulated, and the results show that the morphing process will change the dynamic aeroelastic stability, and the influences of the folding and unfolding processes are opposite.",
keywords = "Aeroelastic, Folding wing, Time variant system",
author = "Wei Hu and Zhichun Yang and Yingsong Gu",
year = "2016",
language = "英语",
series = "30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016",
publisher = "International Council of the Aeronautical Sciences",
booktitle = "30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016",
note = "30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016 ; Conference date: 25-09-2016 Through 30-09-2016",
}