<?xml version="1.0" encoding="UTF-8"?>
<xml>
<records>
<record>
  <contributors>
    <authors>
      <author>Barroso, Jorge</author>
      <author>Jordi Renau, Jordi</author>
      <author>Lozano, Antonio</author>
      <author>Miralles, José</author>
      <author>Martín, Jesús</author>
      <author>Sánchez, Fernando</author>
      <author>Barreras, Félix</author>
    </authors>
  </contributors>
  <titles>
    <title>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</title>
    <secondary-title>Appl. therm. eng.</secondary-title>
  </titles>
  <doi>10.1016/j.applthermaleng.2015.06.003</doi>
  <pages/>
  <volume/>
  <number/>
  <dates>
    <year>2015</year>
    <pub-dates>
      <date>2015</date>
    </pub-dates>
  </dates>
  <abstract/>
</record>

</records>
</xml>