The numerical calculation of subcritical steady potential flow around an unyawed ellipsoid

Show simple item record

dc.contributor.author P. W. Duck en_US
dc.date.accessioned 2014-10-21T15:51:27Z
dc.date.available 2014-10-21T15:51:27Z
dc.date.issued 1975 en_US
dc.identifier.other ARC/R&M-3795 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3074
dc.description.abstract The problem of a subcritical, potential, steady, three-dimensional flow past an unyawed ellipsoid is considered, using ellipsoidal coordinates. The full equations of motion and the exact body surface boundary condition are used throughout. Further, by means of a simple transformation the entire flow field is taken into the computation. A finite difference method, followed by an iterative process is used for the solution of the flow equations. Mach number distributions are given for a number of examples, for the free-stream flow aligned along either the major axis, or the second major axis of the ellipsoid. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title The numerical calculation of subcritical steady potential flow around an unyawed ellipsoid en_US


Files in this item

This item appears in the following Collection(s)

Show simple item record

Search AERADE


Browse

My Account