Electromagnetic-Thermal Integrated Design Optimization for Hypersonic Vehicle Short-Time Duty PM Brushless DC Motor

Table 2

Analytical and FEA results of different designs ( and are the analytical and FEA winding temperature rise).

Designs		(T)	(°C)	(°C)
C1	0.43	1.1	75.4	73.0
C2	0.43	1.3	67.6	66.9
C3	0.43	1.5	63.8	63.0
C4, R3	0.43	1.7	62.0	60.6
R1	0.25	1.7	85.4	82.0
R2	0.35	1.7	65.5	63.0
R4	0.55	1.7	69.5	68.3
R5	0.65	1.7	98.9	97.9