Damage caused by the impact of a foreign object on the turbine blades is caused by the entry of millimeter-sized foreign particles such as sand, stones, or small pieces of broken parts. Consequently, the remaining damage resulting from the impact of a foreign body on the blades is in the form of geometrical discontinuities such as craters or grooves on the blades, which create suitable conditions for the creation and growth of cracks and the complete failure of the blades. One of the most important aspects of foreign body impact damage is the study of the resulting residual stresses at the impact site, which plays a significant role in the creation and growth of cracks. In the present article, the main aim of this work was to analyze the residual stresses due to foreign object damage by expanding the simulation on the blades, considering a real blade model as well as the leading-edge curvature effect. To validate the numerical modeling, the impact of a spherical particle on a flat plate was modeled and the residual stresses and damages resulting from the modeling were compared to the experimental results available in the articles. Finally, the impact of the spherical foreign body on different places of the leading edge of a blade with different impact velocities was investigated. Moreover, the examined blade sample was replaced with a plate with the same material, and the impact of the foreign object on the flat surface was modeled for two different service temperatures. In this study, the resulting residual stresses and strains in three critical areas were compared.