This paper mainly expounds the aerodynamic design, CFD simulation, wind tunnel experiment, flight test of the total static pressure probe in the high-speed aircraft. The compensation surface of the total static pressure probe can be rapidly adjusted in the design phase through revolution body theory. It concludes the simulation of the static pressure through the commercial CFD software. The aerodynamic performance of the total static pressure probe that is designed should be verified through the wind tunnel test, and it should be ultimately verified whether it meets the requirements or not through the flight test.