2009
DOI: 10.1007/s00707-009-0238-4
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Generalized thermoelastic waves in spherical curved plates without energy dissipation

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Cited by 19 publications
(3 citation statements)
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“…Othman and Singh [16] have studied the equations of a 2-D problem in a micro-polar thermoelastic medium for a half-space whose surface is free and subjected to an instantaneous thermal point source. Jiangong and Tonglong [12] have used the G-N generalized thermoelastic theory without energy dissipation to investigate the propagation of thermoelastic waves in orthotropic spherical curved plates subjected to stress-free, isothermal boundary conditions. Mukhopadhyay and Kumar [15] have formulated the state-space approach to the problems of thermoelastic interactions on the basis of the G-N theory of generalized thermoelasticity of type-III with energy dissipation.…”
Section: Introductionmentioning
confidence: 99%
“…Othman and Singh [16] have studied the equations of a 2-D problem in a micro-polar thermoelastic medium for a half-space whose surface is free and subjected to an instantaneous thermal point source. Jiangong and Tonglong [12] have used the G-N generalized thermoelastic theory without energy dissipation to investigate the propagation of thermoelastic waves in orthotropic spherical curved plates subjected to stress-free, isothermal boundary conditions. Mukhopadhyay and Kumar [15] have formulated the state-space approach to the problems of thermoelastic interactions on the basis of the G-N theory of generalized thermoelasticity of type-III with energy dissipation.…”
Section: Introductionmentioning
confidence: 99%
“…Hosseini and Abolbashari (2010) proposed general analytical solution for elastic radial wave propagation and dynamic analysis of functionally graded thick hollow cylinders subjected to impact loading. Jiangong and Tonglong (2010) studied generalized thermoelastic waves in spherical curved plates without energy dissipation. Othman and Abbas (2012) discussed thermal shock problem in a non-homogeneous isotropic hollow cylinder with energy dissipation.…”
Section: Introductionmentioning
confidence: 99%
“…In the high velocities of modern aircraft give rise to aerodynamic heating, which produces intense thermal stresses that reduce the strength of the aircraft structure. The counterparts of our problem in the contexts of the thermoelasticity theories have been considered by using numerical and analytical methods (Mukhopadhyay, 2006;Mukhopadhyay and Kumar, 2009;Jiangong and Tonglong, 2010;Kumar and Chawla, 2010;Abbas et al, 2011;Abo-Dahab and Abbas, 2011;Abbas, 2011;2012;2013;2014a;2014b;2014c;Abbas and AboDahab, 2014;Abbas and Zenkour, 2014). In which, Abbas solved different problems by eigenvalue approach in the Laplace transformation domain.…”
Section: Introductionmentioning
confidence: 99%