Parametric aeroelastic modeling based on component modal synthesis and stability analysis for horizontally folding wing with hinge joints
Crossref DOI link: https://doi.org/10.1007/s11071-017-3956-5
Published Online: 2018-03-01
Published Print: 2018-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Zhang, Wei
Lv, Shengli
Ni, Yingge
Text and Data Mining valid from 2018-03-01
Article History
Received: 13 April 2017
Accepted: 18 November 2017
First Online: 1 March 2018