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The aerodynamic model of Flush Airdata Sensing System is derived from blunt forebodies, but whether the model is suitable for cone forebodies does not be confirmed. The applicability of the aerodynamic model is verified for a typical cone forebody, and the verification results of the applicability demonstrate that the relative errors of the dynamic pressure and static pressure are more than 2.5% when the aerodynamic model is applied to cone forebody model. Therefore, a modified calibration algorithm for cone forebodies is proposed, and the corresponding validation of simulation is accomplished. Simulation results show that the relative errors of the dynamic pressure and static pressure are less than 0.5%, and the modified calibration algorithm eliminates the model errors effectively.