Simulation effect of hot gas impingement on nacelle lip skin

dc.contributor.author	Mohammad Harith Yaccob Syed
dc.date.accessioned	2021-05-18T02:54:11Z
dc.date.available	2021-05-18T02:54:11Z
dc.date.issued	2017-06
dc.description.abstract	Ice accumulation during flight includes the accumulation of icing on the nacelle lip skin of the aircrafts engines. The accumulation on the ice on the inner surface of the lipskin can be hazardous to any flying aircraft [2]. Computational Fluid Dynamics (CFD) has been widely used to study the effect of ice accretion onto the nacelle lip skin. This study however utilizes the fluid structure interaction (FSI) to study the effect of hot gas impingement on the nacelle lip skin towards the thermal properties of the material. It was found that the material used for this study, AL 1 series, 2 series and 7 series has a temperature dependent behavior which is closely related to their microscopic properties. This study has shown that the tensile strength of the materials decreases as the temperature increases and this study also has concluded that aluminum 7 series is the most suitable material to be used for the nacelle lip skin material.	en_US
dc.identifier.uri	http://hdl.handle.net/123456789/13465
dc.language.iso	en	en_US
dc.title	Simulation effect of hot gas impingement on nacelle lip skin	en_US
dc.type	Other	en_US

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