33th Congress of the International Council of the Aeronautical Sciences

03.1 - Aerodynamics – CFD Methods and Validation

DEVELOPMENT OF A CFD MODEL AND METHODOLOGY FOR THE INTERNAL FLOW SIMULATION IN A HYDROGEN-POWERED UAV

A. Porcarelli, KTH - Royal Institute of Technology, Sweden

The onboard carrying of a hydrogen fuel cell leads to unexplored internal flow characteristics, including the introduction of water vapour. Given the strict environmental operational requirements of PEM fuel cells, a Runge-Kutta-based solver is developed and tested to effectively assess the evolution of the UAV internal bay flow temperature and humidity fields.


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