Numerical simulation study on temperature field of helicopter nacelle fire under non-ventilation condition
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Numerical simulation study on temperature field of helicopter nacelle fire under non-ventilation condition
Vol. 26, Issue 8, (2011)
作者机构:
北京航空航天大学 航空科学与工程学院,北京,100191
作者简介:
基金信息:
DOI:
CLC:
Published:2011
稿件说明:
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NIU Xue-min, XIE Yong-qi, YU Jian-zu. Numerical simulation study on temperature field of helicopter nacelle fire under non-ventilation condition[J]. 2011, 26(8).
DOI:
NIU Xue-min, XIE Yong-qi, YU Jian-zu. Numerical simulation study on temperature field of helicopter nacelle fire under non-ventilation condition[J]. 2011, 26(8).DOI:
Numerical simulation study on temperature field of helicopter nacelle fire under non-ventilation condition
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.