Boundary layer flows induced due to retarded motion of the continuous surfaces ultimately seize at some subsequent downstream location which is equivalent to the phenomenon of flow separation on a surface of finite length, thus leading to increased drag on the aero-dynamical vehicles. The literature has established that the boundary layer formed over a moving continuous surface is more energetic than that formed on a stationary surface of finite length. This implies that for the sustainability of the transport phenomenon in such a retarded flow, which has to ultimately meet the flow separation, a moving continuous surface is preferable to a stationary surface of finite length. Therefore, this study intends to perform heat transfer analysis in a retarded laminar boundary layer formed due to a moving continuous cylinder of constant radius. Wall temperature of uniform nature is considered in this investigation. In the majority of the boundary layer flows the self-similarity of the flow does not persist because of choosing the reference velocity of the desired character. Thus, the problem becomes non-similar in nature. In general, the non-similarity of a flow may appear due to various aspects of the problem such as the retarded nature of the reference velocity, the surface temperature, the curvature of the body, etc. Surface transverse curvature imparts favorable consequences on the separating boundary layer and hence on the seizing flow character. Therefore, this study focuses on investigating the impact of surface transverse curvature (TVC) k and the wall velocity power index m on temperature profiles, rate of heat transfer at the surface Nux(local Nusselt number), the thermal layer thickness, and the thermal diffusivity of heat in a retarded boundary layer. In addition to this, the influence of Prandtl number Pr and Stanton number St has also been investigated.