Investigation of heat transfer characteristics of aircraft icing under runback water
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Investigation of heat transfer characteristics of aircraft icing under runback water
Vol. 24, Issue 9, (2009)
作者机构:
中国空气动力研究与发展中心,绵阳,621000
作者简介:
基金信息:
DOI:
CLC:
Published:2009
稿件说明:
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DU Yan-xia, GUI Ye-wei, XIAO Chun-hua, et al. Investigation of heat transfer characteristics of aircraft icing under runback water[J]. 2009, 24(9).
DOI:
DU Yan-xia, GUI Ye-wei, XIAO Chun-hua, et al. Investigation of heat transfer characteristics of aircraft icing under runback water[J]. 2009, 24(9).DOI:
Investigation of heat transfer characteristics of aircraft icing under runback water
The heat transfer characteristics of aircraft icing process were investigated based on the theories of liquid-solid phase change and film flowing.The heat transfer model which coupled runback water flowing with liquid-solid phase change was established and the influence of airflow parameters on the characteristics of icing growth was analyzed.The results indicate that the runback water on the icing surface will accelerate the liquid-solid phase change and speed up the icing process.The shear stress caused by the airflow is the key factor to the runback water flowing.The higher the airflow speed
the greater the shear stress and stronger the runback water flowing becomes
and vice versa.Under the condition of runback water flowing
the speed and temperature of the airflow are the main causes affecting the icing accretion.The higher the airflow speed or the lower the temperature
the greater the icing rate will be.The liquid water content and the collection efficiency have weak effect on the icing rate comparatively.