The current study combines a solution for the displacement examination of fundamentally simply supported one, trilogy, and quadruple coat laminated layers with uniformly distributed load using a hyperbolic shear deformation theory that considers thermal impact. Higher shear deformation theory with dislodging field over the beam crossarea yields these beam mathematical results. The thickness of a laminated beam is used to determine the course of action of a beam, which is handled by a rule of virtual work procedure. The standard of imaginary work is utilized to administer divergent circumstances along with cut-off states for beams. In light of shear distortion, verbalizations for cross over removal of beams are obtained, as well as responsibility. MATLAB coding was used to manage the mathematical findings for aspect rations and thickness extents. To confirm the precision of the result, the current exploration's results are compared to those of other shear deformation theories

Displacement, Laminated beam, MATLAB Coding, Temperature effect, Hyperbolic Shear Deformation Theory