What is it about?
Thermal management of batteries on (hybrid) electric aircraft is difficult due to the high heat loads in combination with the restricted operating temperatures of the batteries. We develop a model of the entire thermal management system and design a cooling system for a small 19 passenger electric aircraft.
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This page is a summary of: Design of a Battery Cooling System for Hybrid Electric Aircraft, Journal of Propulsion and Power, May 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b38695.
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