The numerical solution of certain differential equations occurring in Crocco's theory of the laminar boundary layer

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dc.contributor.authorKirkby, S.
dc.contributor.authorNonweiler, T.
dc.date.accessioned2012-09-11T13:24:36Z
dc.date.available2012-09-11T13:24:36Z
dc.date.issued1953-05
dc.description.abstractA numerical method is described for the solution of certain differential equations which result from the application of Crocco’s transformation to the laminar boundary layer equations appropriate to high supersonic Mach numbers. (i.e. at hypersonic speeds). Continues …en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7562
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfielden_UK
dc.relation.ispartofseriesCollege Reportsen_UK
dc.relation.ispartofseries74en_UK
dc.titleThe numerical solution of certain differential equations occurring in Crocco's theory of the laminar boundary layeren_UK
dc.typeReporten_UK

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