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Dynamic analysis of an aeroelastic airfoil with freeplay nonlinearity by precise integration method based on Padé approximation

Crossref DOI link: https://doi.org/10.1007/s11071-017-3577-z

Published Online: 2017-05-27

Published Print: 2017-08

Update policy: https://doi.org/10.1007/springer_crossmark_policy

Authors

Tian, Wei

Yang, Zhichun

Gu, Yingsong
Funding

Funding for this research was provided by:

National Natural Science Foundation of China (11472216)

National Natural Science Foundations of China (11672240)

111 Project of China (B07050)
License Information

License valid from 2017-05-27