The invention discloses a disturbance region updating method of steady compressible flow, and belongs to the technical field of computational fluid mechanics. The method includes steps of input file loading, flow field initialization, dynamic-computation-domain establishment, boundary virtual-grid updating, dynamic-computation-domain updating, residual estimation, time integration, judgment of whether convergence occurs and result output. The method is suitable for use in solving of any compressible flow on the basis of a time-propulsion method, can be combined with any spatial discrete formatand time-propulsion format and other existing time-propulsion acceleration technology, and is suitable for use in different initialization methods and complex and discontinuous wall surface conditions. The method can greatly improve calculation efficiency; for the subsonic-speed flow problem, the method can reasonably remove redundant far-field units in a later stage of solving near a steady state, and effectively narrow a computational domain; and for the supersonic-speed flow problem, the method can also reduce a storage requirement of a solving process.