“…1 includes Heights of the barriers (h b1 , h b2 , h b3 ), Length of the barriers (l b1 , l b2 , l b3 ), Angular positions at airgap, (∆δ 1 , ∆δ 2 , ∆δ 3 ) defined with respect to centre of the shaft, Flux barrier tip angles (β 1 , β 2 , β 3 ) measured between the ends of the flux barriers, defined with respect to centre of the shaft, Iron rib thickness(t i ), the thickness between the end of the flux barriers and periphery of the rotor and Air gap length (a g ). The lamination of the prototype rotor used for analysis is based on significant contributions made in [3,12,26], and is shown in Fig. 2.…”