Publication | Open Access

Experimental determination of the heat transfer coefficient for the optimal design of the cooling system of a PEM fuel cell placed inside the fuselage of an UAV

Heat Transfer ProcessEngineeringThermal ProtectionAerospace EngineeringEnergy EfficiencyHeat ExchangerHeat Transfer CoefficientThermal ManagementOptimal DesignTransport PhenomenaThermal ModelingThermodynamicsHeat TransferThermal EngineeringPem Fuel Cell