Because of the relative ease of balancing round rotors, and their ability to withstand high centrifugal forces, round-rotor generators are more stable and normally used for turbo units driven by high-speed steam or gas turbines. Generators operating at a lower speed, such as those driven by hydro turbines, need many magnetic poles in order to operate at 50 or 60 Hz. As the centrifugal forces experienced by the rotors of these low-speed machines are lower than in the corresponding turbo generators, salient poles can be used and the rotor diameter increased.
The torque developed in a salient-pole generator consists of two components.
The first component, proportional to sin δ, is identical to the torque expressed by Equation below for a round-rotor generator and is termed the synchronous torque.
The second component, termed the reluctance torque, arises as the rotor tries to assume a position of minimum magnetic reluctance by moving towards the air-gap mmf. This additional torque is due to the non-uniform air gap and is a direct consequence of the air-gap mmf and flux not being in phase. The reluctance torque is present even without any field excitation and is proportional to sin 2δ. It vanishes for both δ = 0 and δ = π/2.
As you know from single generator stability theory (equal - area criterion), The areas A1 (figure below) is directly proportional to the increase in kinetic energy of the rotor while it is accelerating, whereas areas A2 is proportional t o the decrease in kinetic energy of the rotor while it is decelerating. Therefore, the equal - area criterion states that the kinetic energy added to the rotor following a fault must be removed after the fault in order to restore the rotor to synchronous speed.
The shaded area A1 is dependent on the time taken to clear the fault. If there is delay in clearing, the angle δc is increased; likewise, the area A2 increases and the equal-area criterion requires that area A2 also increase to restore the rotor to synchronous speed at a larger angle of maximum swing δx.
Generally comparing between the round and salient-pole rotor power curve, we expect smaller area A2 in salient-pole and area A1 in round case resulting deformation of power curve to left side as illustrated below. Therefore it seems performance stability of round rotor is better in fault conditions.