Równania Powłoki Stożkowej Trójwarstwowej Wewnątrz Użebrowanej z Lekka Warstwą Wypełniającą
Abstract
Equations of equilibrium of three-layer conical shell are derived. After the determination of the displacement strains and stresses at any point of the shell the variational method is used thus obtaining a system of five equations. For a certain case of load, after the derivation of the AIRY function, a system of four partial differential equations is obtained, from which it is easy in the case of a cylindrical shell to pass to a system of two differential equations obtained by GRIGOLYUK and determining the stress function and the deflection function.References
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[9] E. REISSNER, Finite Deflection of Sandwich Plates, J. Aeron Sci., 7, 15 (1948), 435-440.
[10] E. REISSNER, Errata, Finite Deflection of Sandwich Plates, J. Aeron. Sci., 2, 17 (1950), 125.
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[9] E. REISSNER, Finite Deflection of Sandwich Plates, J. Aeron Sci., 7, 15 (1948), 435-440.
[10] E. REISSNER, Errata, Finite Deflection of Sandwich Plates, J. Aeron. Sci., 2, 17 (1950), 125.
[11] [in Russian]
[12] [in Russian]