30th Congress of the International Council of the Aeronautical Sciences

06 - Systems, Subsystems and Equipment

COUPLED EMC-THERMAL MODELING OF ELECTRICAL HARNESSES WITHIN "MORE ELECTRICAL AIRCRAFT"

F. Mahiddini¹, M. Ridel¹, P. Reulet¹, D. Donjat¹, P. Millan¹; ¹ONERA, France

The link between fundamental equations of Heat Transfer and ElectroMagnetic Compatibility allows the simultaneous computation of Thermal and EMC constraints at harness level, meaning a huge interest in the framework of More Electrical Aircraft developments. An original method, based on geometrical properties of the Poisson's equation, could lead to a precise and fast computation of both of them.


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