The compressible laminar boundary layer with foreign gas injection

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dc.contributor.authorCraven, A. H.
dc.date.accessioned2014-12-08T09:58:14Z
dc.date.available2014-12-08T09:58:14Z
dc.date.issued1962-01
dc.description.abstractThe 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.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/8861
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCollege of Aeronautics Reportsen_UK
dc.relation.ispartofseries155en_UK
dc.relation.ispartofseriesCOA/155en_UK
dc.titleThe compressible laminar boundary layer with foreign gas injectionen_UK
dc.typeReporten_UK

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