Slip flow past slender pointed bodies

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dc.contributor.authorStribling, C. B.
dc.date.accessioned2014-12-08T10:45:45Z
dc.date.available2014-12-08T10:45:45Z
dc.date.issued1963-05
dc.description.abstractUsing Oseen's approximation to linearise the Navier-Stokes equations, a solution to the problem of axisymmetric slip flow past slender bodies of revolution at zero incidence has been obtained, in a manner similar to that used by Laurmann in his paper on the slip flow past a flat plate(6). The drag coefficient has been evaluated for both incompressible and compressible flows, and this has been compared with normal boundary layer values. It is found that the skin friction drag is the dominant component of drag in the incompressible case and in the compressible case.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/8866
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCollege of Aeronautics Reportsen_UK
dc.relation.ispartofseries160en_UK
dc.relation.ispartofseriesCOA/160en_UK
dc.titleSlip flow past slender pointed bodiesen_UK
dc.typeReporten_UK

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