The development of a simple method for drag estimation for wedge-like fairings in hypersonic flow

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dc.contributor.authorRoussel, Alexandre
dc.contributor.authorPrince, Simon A.
dc.contributor.authorViguer, Matthieu
dc.contributor.authorKshitij, Abhinav
dc.contributor.authorStollery, John
dc.contributor.authorGarry, Kevin
dc.date.accessioned2019-10-14T14:03:03Z
dc.date.available2019-10-14T14:03:03Z
dc.date.issued2016-09-30
dc.description© The Authors
dc.description.abstractThe addition of wedge-like fairings onto the side of missiles and space launch vehicles, to shield devices such as cameras or reaction jet nozzles, creates additional drag, particularly when in supersonic/hypersonic flow. An experimental and computational study was performed to obtain data on wedge configurations and develop simple theories for the drag due to these types of fairings.en_UK
dc.identifier.citationRoussel A, Prince SA, Viguer M, et al., (2016) The development of a simple method for drag estimation for wedge-like fairings in hypersonic flow. Proceedings of 30th Congress of the International Council of the Aeronautical Sciences, 25-30 September 2016, Daejeon, Koreaen_UK
dc.identifier.isbn9781510834552
dc.identifier.urihttp://www.icas.org/ICAS_ARCHIVE/ICAS2016/data/preview/2016_0244.htm
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/14613
dc.language.isoenen_UK
dc.publisherICASen_UK
dc.rights© The Authors
dc.titleThe development of a simple method for drag estimation for wedge-like fairings in hypersonic flowen_UK
dc.typeConference paperen_UK

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