Abstract For a shell with three sections, dependences of the critical frequency on the different thicknesses of these sections are obtained. The error of the assumptions accepted at constructing the mathematical model of a shell is evaluated.
Dynamic Stability of an Orthotropic Cylindrical Shell of Piecewise Constant Thickness under the Action of External Pulsating Pressure
Russian Aeronautics ; 62 , 2 ; 192-198
01.04.2019
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Dynamic Stability of a Cylindrical Shell under Alternating Axial External Pressure
Springer Verlag | 2017
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