The principle of constructing a computation model of equilibrium ribbed stiffened shells in linear displacement-based FEM analysis
Russian aeronautics ; 56 , 2
2013
Article (Journal)
English
BKL: | 55.50 Luftfahrzeugtechnik | |
Local classification TIB: | 770/7040/8000 |
Tema Archive | 1979
|Synthesis of Stiffened Conical Shells
AIAA | 1972
|Dynamic response analysis of stiffened conoidal shells
Online Contents | 2006
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