Nose controls on delta wings at supersonic speeds

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dc.contributor.authorBolton Shaw, B. W.
dc.date.accessioned2012-06-08T10:51:57Z
dc.date.available2012-06-08T10:51:57Z
dc.date.issued1950-05
dc.description.abstractExpressions are derived for lξ and a2 of nose ailerons and nose elevators on a delta wing, as depicted in Fig. 1, in supersonic flight. Nose and trailing edge controls on delta wings in supersonic flight are compared.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7206
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfield.en_UK
dc.relation.ispartofseriesCollege Reporten_UK
dc.relation.ispartofseries36en_UK
dc.titleNose controls on delta wings at supersonic speedsen_UK
dc.typeReporten_UK

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