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- W2392728146 abstract "The temperatures of an engine nacelle installed in an helicopter exceed the limited value in rear-nacelle in hoverflight test on ground, therefore, The calculation models of fluid flow and heat transfer of the engine nacelle are created. The flow and temperature fields are computed when engine is operating under ground maximum state, and the results indicate that the temperatures of monitoring points exceed certain value. Two schemes are presented to improve nacelle structure; the flow and temperature fields are calculated respectively. The results show that the effects of flow and temperature fields have been improved in some extent compared with the original one; and the temperatures of monitoring points are less than the limited value. The schemes presented in this paper are effective on engineering application." @default.
- W2392728146 created "2016-06-24" @default.
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- W2392728146 date "2008-01-01" @default.
- W2392728146 modified "2023-09-25" @default.
- W2392728146 title "Fluid flow and heat transfer calculation on an engine nacelle" @default.
- W2392728146 hasPublicationYear "2008" @default.
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