An investigation of boundary layer effects on two dimensional supersonic aerofoils

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dc.contributor.authorZienkiewicz, H. K.
dc.date.accessioned2012-07-04T11:12:03Z
dc.date.available2012-07-04T11:12:03Z
dc.date.issued1951-12
dc.description.abstractThe phenomena of viscous flow over two-dimensional supersonic aerofoils are investigated with a view to developing a method for estimating their effects in the aerodynamic characteristics of the aerofoils. Continues …en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7338
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfielden_UK
dc.relation.ispartofseriesCollege Reporten_UK
dc.relation.ispartofseries49en_UK
dc.titleAn investigation of boundary layer effects on two dimensional supersonic aerofoilsen_UK
dc.typeReporten_UK

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