Abstract
A method is described applicable to the analysis of the carrying capacity of flat or curved panels, made of composite materials, under biaxial tension with shear. The design of a test apparatus is shown, and the errors in simulating a given load distribution on it are evaluated.
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Literature cited
F. P. Belyankin, V. F. Yatsenko, and G. G. Margolin, in: Strength and Deformability of Glass Plastics under Biaxial Compression [in Russian], Kiev (1971), p. 21.
P. M. Ogibalov et al., Structural Polymers [in Russian], Vol. 1, Moscow (1972), p. 123.
Yu. M. Tarnopol'skii (editor), Static Method of Testing Reinforced Plastics [in Russian], Riga (1972), p. 134.
A. N. Baranov et al., Static Testing of Supersonic Aircraft for Strength [in Russian] (1974) (in print).
Additional information
Professor N. E. Zhukovskii Central Institute of Aerohydrodynamics, Moscow. Translated from Mekhanika Polimerov, No. 6, pp. 1065–1070, November–December, 1974.
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Belozerov, L.G., Dzhankhotov, S.O. & Kireev, V.A. Analysis of the carrying capacity of panels under biaxial tension with shear. Polymer Mechanics 10, 917–921 (1974). https://doi.org/10.1007/BF00856242
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DOI: https://doi.org/10.1007/BF00856242