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- W1979707875 abstract "The considered investigation was conducted as part of an effort to reduce aircraft fuel costs. Turboprops are very fuel efficient at speeds below Mach 0.6. One of the most promising approaches to reduce fuel consumption in the speed range from Mach 0.6 to 0.8 is related to an employment of the swept eight to ten blade propeller (propfan) being developed by NASA. All studies to date indicate that turboshaft engines with propfans might save 15% or more of the fuel used by a turbofan engine of comparable technology. Attention is given to a turboprop status review, contractor studies, the NASA propfan program, an in-house performance study, specific problems which have to be solved to make a twin-turboprop, 100-150 passenger transport a viable possibility for the early 1990s, and turboprop dilemmas." @default.
- W1979707875 created "2016-06-24" @default.
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- W1979707875 date "1981-08-11" @default.
- W1979707875 modified "2023-09-24" @default.
- W1979707875 title "Wright Field turboprop study" @default.
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- W1979707875 doi "https://doi.org/10.2514/6.1981-1685" @default.
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