Stress–strain analysis of a thin-shell part of fuselage using a triangular finite element with lagrange multipliers
Crossref DOI link: https://doi.org/10.3103/S1068799816030041
Published Online: 2016-12-29
Published Print: 2016-07
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Klochkov, Yu. V.
Nikolaev, A. P.
Vakhnina, O. V.
Kiseleva, T. A.
License valid from 2016-07-01