On wings with non-elliptic lift distributions

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dc.contributor.authorBragado-Aldana, Estela
dc.contributor.authorLone, Mudassir
dc.contributor.authorRiaz, Atif
dc.date.accessioned2022-07-29T11:47:12Z
dc.date.available2022-07-29T11:47:12Z
dc.date.issued2021-09-10
dc.description© The Author.
dc.description.abstractNon-elliptic lift distributions were originally conceived by Prandtl as a solution for wings having optimal aerodynamic and structural efficiency. Since 1933, many researchers have expanded on this theory to confirm that it explicitly facilitates the trade-off between induced drag and weight, and have unveiled other potential benefits such as proverse yaw. This theory is seen as a promising alternative to redefine the underlying principles of conceptual wing design in the search for a step increase in efficiency. Given the recent revival of this approach, in this paper the authors present a concise review of its theoretical basis, the developments carried out in this area and their relevance to the future of aviation.en_UK
dc.identifier.citationBragado-Aldana E, Lone MM, Riaz A. (2021) On wings with non-elliptic lift distributions. In: ICAS 2021: 32nd Congress of the International Council of the Aeronautical Sciences, 6-10 September 2021, Shanghai, Chinaen_UK
dc.identifier.doi10.57996/cran.ceres-1322
dc.identifier.isbn978-3-932182-91-4
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/18259
dc.identifier.urihttps://www.icas.org/ICAS_ARCHIVE/ICAS2020/data/papers/ICAS2020_0253_paper.pdf
dc.identifier.urihttps://doi.org/10.57996/cran.ceres-1322
dc.language.isoenen_UK
dc.publisherICASen_UK
dc.rights© The Authors.
dc.rightsAttribution 4.0 International
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectNon-elliptic lift distributionsen_UK
dc.subjectwing designen_UK
dc.subjectaero-structural efficiencyen_UK
dc.subjectinduced dragen_UK
dc.subjectproverse yawen_UK
dc.titleOn wings with non-elliptic lift distributionsen_UK
dc.typeConference paperen_UK

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