“…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.…”