To avoid surge in centrifugal compressors and blowers always operate at at a flowrate which is higher than the "surge-line" flow. The surge line is generally determined by impeller incidence angle and is more or less independent of rotational speed. For example, if surging is initiated at 30% rated flow at maximum running speed, it will occur at or near 30% of the corresponding rated flow at lower running speeds where rated flow at any running speed is directly proportional to the speed fraction.
Surge in compressible flow turbomachines is generally preceded by blade stall as flow is reduced from rated flow. Since airfoil blade stalling usually occurs at inlet positive incidence angles of roughly 12 to 18 degrees, surge can be expected at incidence angles higher than that.