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- W2316451230 abstract "This study configures a future commercial transport aircraft for a world with expensive fuel. This aircraft was configured for minimum fuel burn, maximizing specific range over a 1000nM reference mission. The design goals align with NASA’s N+1 study objectives: low emissions, transcontinental range, and unrestricted operations from airports such as LGA, BUR or DCA. The Arizona State University aircraft employs current and near-term available technology, but through careful design choices and an unusual flight mission profile, is expected to offer a further 15% reduction in fuel burn from the advanced technology 737-MAX or Airbus 320neo. The most efficient design was found incorporating high-bypass ratio, near-stoichiometric turbofan engines into an otherwise conventional, but high-aspect-ratio wing-body-tail configuration. The minimum fuel burn objective led the team to design an aircraft that flies most efficiently very high and very fast: the design features a long-range cruise speed of Mach 0.83 at an altitude of 46,000-ft. The high thrustto-weight ratio needed to attain efficient cruise gives this aircraft exceptional field performance and low altitude climb capability." @default.
- W2316451230 created "2016-06-24" @default.
- W2316451230 creator A5005505696 @default.
- W2316451230 date "2013-08-08" @default.
- W2316451230 modified "2023-09-23" @default.
- W2316451230 title "High Altitude Hot Rod - An Energy Efficient N+1 Transport" @default.
- W2316451230 cites W1606731623 @default.
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- W2316451230 doi "https://doi.org/10.2514/6.2013-4327" @default.
- W2316451230 hasPublicationYear "2013" @default.
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