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- W2316092521 abstract "The aerodynamic design and test results of the fan and quarter-stage component for the GE/NASA Energy Efficient Engine (EEE) are presented. The fan is a high bypass ratio, single-stage design having 32 part-span shrouded rotor blades, coupled with a unique quarter-stage arrangement that provides additional core-stream pressure ratio and particle separation. The fan produces a bypass pressure ratio of 1.65 at the exit of the low aspect ratio vane/frame and a core-stream pressure ratio of 1.67 at the entrance to the core frame struts. The full-scale fan vehicle was instrumented, assembled and tested as a component in November 1981. Performance mapping was conducted over a range of speeds and bypass ratios using individually-controlled bypass and core-stream discharge valves. The fan bypass and core-stream test data showed excellent results, with the fan exceeding all performance goals at the important engine operating conditions." @default.
- W2316092521 created "2016-06-24" @default.
- W2316092521 creator A5040007199 @default.
- W2316092521 creator A5055636140 @default.
- W2316092521 date "1983-06-27" @default.
- W2316092521 modified "2023-09-24" @default.
- W2316092521 title "The aerodynamic design and performance of the General Electric/NASA EEE fan" @default.
- W2316092521 doi "https://doi.org/10.2514/6.1983-1160" @default.
- W2316092521 hasPublicationYear "1983" @default.
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