The effect of the sweepback of delta wings on the performance of an aircraft at supersonic speeds

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dc.contributor.authorRobinson, A.
dc.contributor.authorDavies, F.T.
dc.date.accessioned2012-05-04T16:58:48Z
dc.date.available2012-05-04T16:58:48Z
dc.date.issued1947-03
dc.description.abstractThe variation with sweepback of total drag of an aircraft in level flight at supersonic speeds is calculated. It is shown that sweepback is not uniformly beneficial, but that in general the optimum amount of sweepback depends in the design speed and altitude.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7119
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfield.en_UK
dc.relation.ispartofseriesCollege Reporten_UK
dc.relation.ispartofseries6en_UK
dc.titleThe effect of the sweepback of delta wings on the performance of an aircraft at supersonic speedsen_UK
dc.typeReporten_UK

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