Nonlinear Deformation and Stability of the Aircraft Fuselage Composite Section under Pure Bending
Crossref DOI link: https://doi.org/10.3103/S106879982103003X
Published Online: 2021-12-11
Published Print: 2021-07
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Zheleznov, L. P.
Serāeznov, A. N.
Text and Data Mining valid from 2021-07-01
Version of Record valid from 2021-07-01
Article History
Received: 2 February 2021
Revised: 17 February 2021
Accepted: 26 February 2021
First Online: 11 December 2021