The dynamic response of doubly curved shell under effect of environment sustainable temperature

The current work aimed to demonstrate the reliability of some engineering applications under hard conditions and thermal environment, which results in failure many structures such as spacecraft components benefit from those order achieve required limits for sustainable development reach best influence environments. according extremely high specific stiffness strength, composite laminates with fiber reinforcement were widely being employed weight sensitively like aeroplanes are transient rectangular sine pressure pulse loads during launch orbit consider highest structure. In situations, a thermo-mechanical become dominant loads, that one factors can on laminate design is their stability. present presents semi-analytical approach (levy-type) by using Matlab 2020 code examine effect orientation response central deflection well normal stress analysis doubly curved shallow shell exposed triangular sinusoidal distributed loading. show various materials, geometric characteristics, boundary temperature have different influences parameters.