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Transient response of cylindrical shells with arbitrary shaped sections
AbstractA new coordinate transformation function is presented, with the help of which a cylindrical shell of arbitrary cross-section can be mapped approximately into a circular cylindrical shell. Using this method, the transient response of a non-circular cylindrical shell subjected to a shock wave is obtained by the finite strip method. The versatility and accuracy of the method are amply demonstrated through a number of numerical examples.
Transient response of cylindrical shells with arbitrary shaped sections
AbstractA new coordinate transformation function is presented, with the help of which a cylindrical shell of arbitrary cross-section can be mapped approximately into a circular cylindrical shell. Using this method, the transient response of a non-circular cylindrical shell subjected to a shock wave is obtained by the finite strip method. The versatility and accuracy of the method are amply demonstrated through a number of numerical examples.
Transient response of cylindrical shells with arbitrary shaped sections
Cheung, Y.K. (Autor:in) / Cao Zhi Yuan (Autor:in) / Zhu Jian Xiong (Autor:in)
Thin-Walled Structures ; 11 ; 305-318
01.12.1989
14 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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