Theoretical stability derivatives of a highly swept delta wing and slender body combination

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dc.contributor.authorNonweiler, T.
dc.date.accessioned2012-07-04T11:23:38Z
dc.date.available2012-07-04T11:23:38Z
dc.date.issued1951-11
dc.description.abstractThe stability derivatives of a delta wing of small aspect ratio, mounted on a cylindrical body with a slender pointed head, are derived by considering the flow in planes perpendicular to the body axis to be uninfluenced by the change in the streamwise component of the air velocity (the so-called ‘slender body’ theory).en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7339
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfielden_UK
dc.relation.ispartofseriesCollege Reporten_UK
dc.relation.ispartofseries50en_UK
dc.titleTheoretical stability derivatives of a highly swept delta wing and slender body combinationen_UK
dc.typeReporten_UK

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