a compressor component having an airfoil with a profile in accordance with table 1 is disclosed . the compressor component , such as a compressor blade , has an increased thickness over a portion of the airfoil span in order to increase stiffness . furthermore , the airfoil has been restacked so as to induce a compressive stress in the blade root / attachment area . the increased stiffness and restacked airfoil combine to improve high - cycle fatigue capability of the compressor component .