Nonlinear metamaterial enabled aeroelastic vibration reduction of a supersonic cantilever wing plate
Crossref DOI link: https://doi.org/10.1007/s10483-024-3165-7
Published Online: 2024-09-30
Published Print: 2024-10
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Sheng, Peng
Fang, Xin
Yu, Dianlong
Wen, Jihong
Text and Data Mining valid from 2024-09-30
Version of Record valid from 2024-09-30
Article History
Received: 13 April 2024
Revised: 3 July 2024
First Online: 30 September 2024
Ethics
: <b>Conflict of interest</b> The authors declare no conflict of interest.