Slip flow past slender pointed bodies

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dc.creator Stribling, C. B.
dc.date 2014-12-08T10:45:45Z
dc.date 2014-12-08T10:45:45Z
dc.date 1963-05
dc.date.accessioned 2022-05-09T10:17:28Z
dc.date.available 2022-05-09T10:17:28Z
dc.identifier http://dspace.lib.cranfield.ac.uk/handle/1826/8866
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/4832
dc.description Using 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.
dc.language en
dc.publisher College of Aeronautics
dc.relation College of Aeronautics Reports
dc.relation 160
dc.relation COA/160
dc.title Slip flow past slender pointed bodies
dc.type Report


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