Wind tunnel measurements of the lift-dependent drag of thin conically cambered slender delta wings at mach numbers 1.4 and 1.8

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dc.contributor.author M. S. Igglesden en_US
dc.date.accessioned 2014-10-20T11:02:40Z
dc.date.available 2014-10-20T11:02:40Z
dc.date.issued 1960 en_US
dc.identifier.other ARC/CP-519 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/532
dc.relation.ispartofseries Aeronautical Research Council Current Papers en_US
dc.title Wind tunnel measurements of the lift-dependent drag of thin conically cambered slender delta wings at mach numbers 1.4 and 1.8 en_US


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