Conceptual design of low-boom low-drag supersonic transports

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dc.contributor.authorSun, Yicheng
dc.contributor.authorSmith, Howard
dc.contributor.authorChen, Haixin
dc.date.accessioned2020-08-11T09:14:27Z
dc.date.available2020-08-11T09:14:27Z
dc.date.issued2020-06-08
dc.description.abstractThis paper introduces a supersonic aircraft design model developed in a multidisciplinary design analysis and optimization (MDAO) environment. Low- to medium- fidelity methods are applied to the conceptual design model. A family of different classes supersonic aircraft are designed with similar general layout, including a single seat supersonic demonstrator, a 10-passenger supersonic business jet and a 50-seat supersonic airliner. These concepts prove the feasibility of low-boom low-drag supersonic transport designs in a multidisciplinary perspective. There are some challenges to balance the volume with packaging and control requirements. The low-boom design for configuration with nacelles are also very challenging.en_UK
dc.identifier.citationSun Y, Smith H, Chen H. (2020) Conceptual design of low-boom low-drag supersonic transports. In: AIAA Aviation 2020 Forum, Virtual Event, 15-19 June 2020en_UK
dc.identifier.isbn978-1-62410-598-2
dc.identifier.urihttps://doi.org/10.2514/6.2020-2635
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/15657
dc.language.isoenen_UK
dc.publisherAIAAen_UK
dc.rightsAttribution-NonCommercial 4.0 International
dc.rights.urihttp://creativecommons.org/licenses/by-nc/4.0/
dc.titleConceptual design of low-boom low-drag supersonic transportsen_UK
dc.typeConference paperen_UK

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