Testing and analysis of a 60 degrees swept back wing with ribs parallel to the line of flight

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dc.contributor.authorHowe, D.
dc.date.accessioned2012-09-13T15:27:37Z
dc.date.available2012-09-13T15:27:37Z
dc.date.issued1953-08
dc.description.abstractThe specimen used in this work represents the load carrying structure of a cambered two spar 60 degree sweptback wing, having closely pitched ribs of large boom area parallel to the line of flight, and thick skins. Continues …en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7578
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfielden_UK
dc.relation.ispartofseriesCollege Reportsen_UK
dc.relation.ispartofseries66en_UK
dc.titleTesting and analysis of a 60 degrees swept back wing with ribs parallel to the line of flighten_UK
dc.typeReporten_UK

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