Design case of the E-19 AEOLUS supersonic business jet

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dc.contributor.authorSmith, Howard
dc.contributor.authorSun, Yicheng
dc.date.accessioned2020-08-11T09:56:11Z
dc.date.available2020-08-11T09:56:11Z
dc.date.issued2020-06-08
dc.description.abstractThis paper introduces the E-19 AEOLUS supersonic business jet designed by the authors (conceptual design) and a team of Staff and a team of graduate students (preliminary and detail design) from the Aerospace Vehicle Design MSc. The design is presented at the 50th anniversary of the first flight of Concorde and with growing interest from many aircraft design companies. An attractive design would still need the usual attributes of safety, security, comfort, reliability, performance and operational flexibility. This paper presents a design that attempts to address these issues. The details of cabin, structures, landing gear, systems, powerplants, etc. are designed. Low-boom low-drag technologies are applied to the design. The synthetic vision display and double drooping nose are introduced to increase the pilot’s field of view. The resulting concept is challenging but could result in an aircraft well suited to meet a new market opportunityen_UK
dc.identifier.citationSmith H and Sun Y. (2020) Design case of the E-19 AEOLUS supersonic business jet. In: AIAA Aviation 2020 Forum, 15-19 June 2020, Virtual Eventen_UK
dc.identifier.isbn978-1-62410-598-2
dc.identifier.urihttps://doi.org/10.2514/6.2020-2618
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/15659
dc.language.isoenen_UK
dc.publisherAIAAen_UK
dc.rightsAttribution 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/*
dc.subjectAircraft designen_UK
dc.titleDesign case of the E-19 AEOLUS supersonic business jeten_UK
dc.typeConference paperen_UK

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