Surface cooler for aero engine
作者： Hong Yu
DOI:
关键词: Aero engine 、 Air channel 、 Air stream 、 Duct (flow) 、 Gas turbines 、 Mechanics 、 Airfoil 、 Geology
摘要: A gas turbine engine has a surface cooler having member defining fluid passage and at least partially contained in an airfoil shaped flow guide member. The is disposed within bypass duct supported on one of the walls. provides smooth outer to main portion air stream passing over cooler, defines inner channel between that supporting walls for secondary pass through channel.
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