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Numerical simulation study on temperature field of helicopter nacelle fire under non-ventilation condition

  • Xue Min Niu*
  • , Yong Qi Xie
  • , Jian Zu Yu
  • *此作品的通讯作者
  • Beihang University

科研成果: 期刊稿件文章同行评审

摘要

The model of fire was established for nacelle of helicopter using large eddy simulation (LES) technology. Taking oil pool fire as an investigation object, the fire scene was designed. Different ignition positions of nacelle fire were studied by simulation method. And the influences of ignition positions on heat release rate, velocity field and temperature field under non-ventilation condition were analyzed. The results show that it has a significant effect on fire propagation in nacelle when the ignition positions are changed. Meanwhile, serious damage of components occurs at the bottom of nacelle in 1/4 position due to strong fire. So, more attention shall be paid to the fire protection design. The conclusion provides a reference for design of fire protection in nacelle.

源语言英语
页(从-至)1761-1767
页数7
期刊Hangkong Dongli Xuebao/Journal of Aerospace Power
26
8
出版状态已出版 - 8月 2011

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