International Journal of Aerospace Engineering / 2016 / Article / Fig 8

Research Article

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

Figure 8

Prototype and measuring instruments. (a) Prototype, controller, and dynamometer. (b) Dynamometer controller, power analyzer, and LCR tester.
(a)
(b)

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