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Analysis of a shell of revolution subjected to axisymmetric loading taking into account geometric nonlinearity on the basis of the mixed finite element method
Gureeva, N. A., Klochkov, Yu. V., Nikolaev, A. P.Volume:
57
Language:
english
Journal:
Russian Aeronautics (Iz VUZ)
DOI:
10.3103/S1068799814030039
Date:
July, 2014
File:
PDF, 499 KB
english, 2014