Abstract
Geometrically nonlinear relationships are derived for thin elastic shells subjected to nonuniform heating. A discrete system describing the thermally stressed state of a shell subject to significant shape variation is obtained using the concept of finite elements. The strain state is determined by the iteration method, based on computation of the first and second variations of the system's energy. Examples are cited for the calculation of a plate with an elliptical heating zone and a shell of canonical shape under nonstationary heating.
Similar content being viewed by others
Literature cited
V. V. Kabanov, Stress-strain state of a stiffened circular cylindrical shell subjected to nonuniform heating and internal pressure, Design of Aircraft Structural Components [in Russian], Mashinostroenie, Moscow (1982), pp. 27–30.
I. E. Muravinskii, “Determination of the stresses and strains in a nonlinearly elastic conical shell subjected to aerodynamic loading and heating,” Prikl. Mekh., No. 6, 64–70 (1984).
M. M. Kornishin and M. M. Suleimanova, “Geometrically and physically nonlinear bending of noninclined shells of different shape under the combined effect of temperature and external forces,” Probl. Prochn., No. 12, 80–83 (1983).
B. Boley and J. Weiner, Theory of Thermal Stresses, Wiley, New York (1960).
P. M. Ogibalov and V. F. Gribanov, Thermal Stability of Plates and Shells [in Russian], Izd. Mosk. Univ., Moscow (1968).
V. V. Kabanov, “Temperature stability of shells,” Prik. Mekh., No. 11, 137–319 (1968).
E. I. Grigolyuk and V. V. Kabanov, Shell Stability [in Russian], Nauka, Moscow (1978).
A. S. Vol'mir, Stability of Deformable Systems [in Russian], Nauka, Moscow (1967).
V. I. Myachenkov and L. A. Pakhomova, “Local stability of cylindrical shells subjected to heating,” Mekh. Tverd. Tela, No. 2, 130–133 (1968).
V. V. Kuznetsov and Yu. V. Soinikov, “Solution of problems of the equilibrium of thin elastic bodies subjected to large displacements and rotations,” Proceedings of the Fourteenth All-Union Conference on the Theory of Plates and Shells (Kutaisi, 1987) [in Russian], Vol. 2, Tbilisskii Universitet, Tbilisi (1987), pp. 110–115.
V. V. Kuznetsov and Yu. V. Soinikov, “Numeric solution of problems of the nonlinear bending of plane rods,” Prikl. Mekh., No. 10, 91–98 (1986).
A. L. Gol'denveizer, Theory of Thin Elastic Shells [in Russian], Gostekhteoretizdat, Moscow (1953).
V. V. Novozhilov, Fundamentals of the Nonlinear Theory of Elasticity [in Russian], Gostekhteoretizdat, Leningrad-Moscow (1948).
P. K. Rashevskii, Course in Differential Geometry [in Russian], Gostekhteoretizdat, Leningrad-Moscow (1950).
J. T. Oden, Finite Elements of Nonlinear Continua, McGraw, New York (1972).
O. Zienkiewicz and I. K. Cheung, Finite Element Method in Engineering Science, McGraw, New York.
Yu. I. Badrukhin, V. V. Kuznetsov, and Yu. V. Soinikov, “Problem of constructing coordinated curved finite elements,” in: Numeric Methods of Solving Problems of the Theory of Elasticity and Plasticity [in Russian], Inst. Teor. Prikl. Mekh. Sib. Otd. Akad. Nauk SSSR, Novosibirsk (1982), pp. 256–261.
Yu. I. Badrukhin, “Calculation of nonstationary temperature fields in the wing of a supersonic aircraft,” in: Design of Aircraft Structural Components [in Russian], Mashinostroenie, Moscow (1982), pp. 13–19.
G. N. Zamula and S. N. Ivanov, “Economic method of calculating nonstationary temperature fields in thin-wall aircraft structures,” Uchen. Zap. Tsentr. Aerogidrodinam. Inst., No. 3, 72–79 (1976).
Author information
Authors and Affiliations
Additional information
Translated from Problemy Prochnosti, No. 10, pp. 69–74, October, 1990.
Rights and permissions
About this article
Cite this article
Kuznetsov, V.V., Soinikov, Y.V. Analysis of the thermally stressed state of shells of arbitrary shape. Strength Mater 22, 1472–1481 (1990). https://doi.org/10.1007/BF00767235
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF00767235