The compressible laminar boundary layer with foreign gas injection

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dc.contributor.author Craven, A. H.
dc.date.accessioned 2014-12-08T09:58:14Z
dc.date.available 2014-12-08T09:58:14Z
dc.date.issued 1962-01
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/8861
dc.description.abstract The equations of the steady compressible two-dimensional laminar boundary layer with foreign gas injection through a porous wall are solved, using an extended form of Lighthill's approximate method, for arbitrary main stream pressure gradient, wall temperature and injection velocity. The wall shear stress and heat transfer rate are obtained in the form of equations suitable for iteration. It is shown that substantial reductions in skin friction and heat transfer rate can be obtained by the injection of a light gas instead of air. en_UK
dc.language.iso en en_UK
dc.publisher College of Aeronautics en_UK
dc.relation.ispartofseries College of Aeronautics Reports en_UK
dc.relation.ispartofseries 155 en_UK
dc.relation.ispartofseries COA/155 en_UK
dc.title The compressible laminar boundary layer with foreign gas injection en_UK
dc.type Report en_UK


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