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A Journal of Russian Academy of Sciences
 Founded
in January 1966
Issued 6 times a year
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IssuesArchive of Issues2020-3pp.423-436

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Yu.I. Vinogradov and G.B. Menkov, "Study of Stress-Strain State of an Aircraft Body at Steering Loads," Mech. Solids. 55 (3), 423-436 (2020)
Year 2020 Volume 55 Number 3 Pages 423-436
DOI 10.3103/S0025654420030164
Title Study of Stress-Strain State of an Aircraft Body at Steering Loads
Author(s) Yu.I. Vinogradov (Bauman Moscow State Technical University, Moscow, 105005 Russia, yuvino@rambler.ru)
G.B. Menkov (Closed Joint Stock Company "Bolid", Moscow, 127018 Russia, gmenkov@narod.ru)
Abstract A design scheme is considered: a cylindrical shell, which is loaded concentrated through the frame. A classical mathematical model is used for the adopted calculation scheme. Based on the mathematical model, the initial problem is analytically solved and an effective algorithm for multiparameter solution of the corresponding boundary value is constructed. The results of a quantitative analysis of the stress-strain state for the aircraft body are presented.
Keywords analytical solution, initial problem, boundary value problem, efficient computational algorithm, parametric analysis
Received 08 November 2019Revised 12 November 2019Accepted 19 November 2019
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