The invention discloses a hypersonic velocity blunt front edge streaming turbulent kinetic energy inlet boundary setting method, which comprises the following steps of S1, calculating a basic flow field, and obtaining a steady basic flow field variable; S2, performing direct disturbance wave simulation by using a numerical simulation system to obtain an unsteady flow field variable; S3, analyzing the flow field to obtain a disturbance field [phi]', and obtaining turbulent energy distribution characteristics; S4, setting a turbulent energy inlet boundary; and S5, calculating turbulence/transition and the like. According to the method, the turbulent energy equation in the turbulence model does not need to be modified, the calculation deviation of the turbulent energy equation at the shock wave downstream can be avoided by setting the inlet boundary condition, the more accurate turbulent energy inlet boundary condition is set based on a direct numerical simulation result, and the method has the advantages of reasonable calculation result, high realizability and high reliability, and can be popularized to three-dimensional flow conditions and the like.