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Investigation of Intake Ducts or a High Speed Subsonic Jet-Propelled Airplane

机译:进气管道或高速亚音速喷气式飞机的研究

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摘要

Effects of roughness, size, and constructional features on efficiency and pressure loss are checked in two intake ducts of different area. Results indicate that larger internal passages increase efficiency. Poor finishing may decrease efficiency by as much as 50%, while spoilers may increase duct pressure los by 700%. Splitter vanes across duct, to insure rigidity, increase pressure loss by about 50%.

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