Ice-Crystal Icing Accretion Studies at the NASA Propulsion Systems Laboratory
Ice-Crystal Icing Accretion Studies at the NASA Propulsion Systems Laboratory
复制标题
美国宇航局推进系统实验室的冰晶积冰研究
DOI:
10.4271/2019-01-1921
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发表时间:
2019
期刊:
影响因子:
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通讯作者:
J. Tsao
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文献类型:
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作者:
P. Struk;J. Agui;T. Ratvasky;M. King;Tadas P. Bartkus;J. Tsao
This paper describes an ice-crystal icing experiment conducted at the NASA Propulsion System Laboratory during June 2018. This test produced ice shape data on an airfoil for different test conditions similar to those inside the compressor region of a turbo-fan jet engine. Mixed-phase icing conditions were generated by partially freezing out a water spray using the relative humidity of flow as the primary parameter to control freeze-out. The paper presents the ice shape data and associated conditions which include pressure, velocity, temperature, humidity, total water content, melt ratio, and particle size distribution. The test featured a new instrument traversing system which allowed surveys of the flow and cloud. The purpose of this work was to provide experimental ice shape data and associated conditions to help develop and validate ice-crystal icing accretion models. The results support previous experimental observations of a minimum melt-ratio threshold for accretion to occur as well as the existence of a plateau region where the icing severity is high for a range of melt ratios. However, a maximum limit for melt ratio, which is suggested in the ice crystal icing literature, was not observed perhaps complicated by the potential for some supercooling of the water at these conditions.
DOI:
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发表时间:
2008
期刊:
History and Philosophy of Science No.21
影响因子:
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作者:
岡本拓司;Takuji OKAMOTO
通讯作者:
Takuji OKAMOTO
DOI:
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发表时间:
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