A Highly Accurate Approach for Aeroelastic System with Hysteresis Nonlinearity

We propose an accurate approach, based on the precise integration method, to solve the aeroelastic system of an airfoil with a pitch hysteresis. A major procedure for achieving high precision is to design a predictor-corrector algorithm. This algorithm enables accurate determination of switching poi...

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Bibliographic Details
Main Authors: C. C. Cui, S. X. Xie, X. C. Huang, J. K. Liu, Y. M. Chen
Format: Article
Language:English
Published: Hindawi Limited 2017-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2017/1459830