Instead of the classical limiting equations of the theory of shells obtained as a result of asymptotic splitting of the initial system, it is proposed to use relations set up by the method of constituent equations. Results of a numerical comparison of calculations made by this method with an exact solution are presented.
机构:
K. E. Tsiolkovskii Inst of Aviation, Technology, Moscow, USSR, K. E. Tsiolkovskii Inst of Aviation Technology, Moscow, USSRK. E. Tsiolkovskii Inst of Aviation, Technology, Moscow, USSR, K. E. Tsiolkovskii Inst of Aviation Technology, Moscow, USSR