Application of a dynamic thermoelastic coupled model for an aerospace aluminium composite panel

An analytical-numerical coupled model has been derived to predict the effects of dynamic thermo-mechanical loading on aluminium composite panels specifically in form metallic skin sandwich structures, for purposes enhanced design spacecraft structures where environmental conditions comprise combined mechanical and thermal loading. The can arise as a consequence localised structural dynamics, is attributable principally solar irradiation eclipse during satellite’s orbit, together they have potential influence de-point adversely, particular. On this basis physics required deal with generalised thermoelastic problem paper reports theoretical work done achieve that. research considered literature detail refined proposed an aerospace application which results solution panels. explored panel under range centrally located static loads, conjunction provided various controlled elevated temperature functions, all prescribed physical boundary conditions. Both forms are shown displacement significantly, thereby confirming importance analysing context.