ISSN 0253-2778

CN 34-1054/N

Open AccessOpen Access JUSTC

A heat transfer empirical correlation for the stratospheric airship based on its length-to-diameter ratio

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https://doi.org/10.3969/j.issn.0253-2778.2013.05.006
  • Received Date: 03 December 2012
  • Rev Recd Date: 26 March 2013
  • Publish Date: 31 May 2013
  • Thermal control is one of the key technologies involved in stratospheric airship applications, and convective heat transfer is an important factor in the thermal control of a stratospheric airship. In order to accurately predict the heat transfer of an airship,using the numerical method, an empirical correlation of Nu number as a function of Re, Pr and l/d (length to diameter ratio) was established. Compared with experimental data, the uncertainty of the empirical correlation is about ±7%. The effect of the attack angle of an airship on heat transfer performance was evaluated. It was found that the heat transfer at the windward side is 10% higher than that of the leeward side, while the average heat transfer of airship is 7% higher when the attack angle changes from 0° to 15°.
    Thermal control is one of the key technologies involved in stratospheric airship applications, and convective heat transfer is an important factor in the thermal control of a stratospheric airship. In order to accurately predict the heat transfer of an airship,using the numerical method, an empirical correlation of Nu number as a function of Re, Pr and l/d (length to diameter ratio) was established. Compared with experimental data, the uncertainty of the empirical correlation is about ±7%. The effect of the attack angle of an airship on heat transfer performance was evaluated. It was found that the heat transfer at the windward side is 10% higher than that of the leeward side, while the average heat transfer of airship is 7% higher when the attack angle changes from 0° to 15°.
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