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IssuesArchive of Issues2008-4pp.610-612

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B. V. Nerubailo, L. G. Smirnov, and O. A. Strukova, "To the solution of the thermoelasticity problem for conical shells," Mech. Solids. 43 (4), 610-612 (2008)
Year 2008 Volume 43 Number 4 Pages 610-612
DOI 10.3103/S0025654408040092
Title To the solution of the thermoelasticity problem for conical shells
Author(s) B. V. Nerubailo (Moscow Aviation Institute (State University of Aerospace Technologies), Volokolamskoe sh. 4, GSP-3, A-80, Moscow, 125993, Russia, borisn@km.ru)
L. G. Smirnov (Moscow Aviation Institute (State University of Aerospace Technologies), Volokolamskoe sh. 4, GSP-3, A-80, Moscow, 125993, Russia)
O. A. Strukova (Moscow Aviation Institute (State University of Aerospace Technologies), Volokolamskoe sh. 4, GSP-3, A-80, Moscow, 125993, Russia, olga544@bk.ru)
Abstract We consider the stress-strain state of thin conical shells in the case of arbitary distribution of the temperature field over the shell. We obtain equations of the general theory based on the classical Kirchhoff-Love hypotheses alone. But since these equations are very complicated, attempts to construct exact solutions by analytic methods encounter considerable or insurmountable difficulties. Therefore, the present paper deals with boundary value problems posed for simplified differential equations. The total stress-strain state is constructed by "gluing" together the solutions of these equations. Such an approach (the asymptotic synthesis method) turns out to be efficient in studying not only shells of positive and zero curvature [1, 2] and cylindrical shells [3] but also conical shells [4, 5]. Here we illustrate it by an example of an arbitrary temperature field, and the problem is reduced to solving differential equations with polynomial coefficients and with right-hand side containing the Heaviside function, the delta function, and their derivatives.
Received 28 May 2007
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