A numerical method for solving the equations for a vortex core

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dc.contributor.author M. G. Hall en_US
dc.date.accessioned 2014-10-21T15:56:34Z
dc.date.available 2014-10-21T15:56:34Z
dc.date.issued 1965 en_US
dc.identifier.other ARC/R&M-3467 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/4046
dc.description.abstract A method is presented for calculating steady axially symmetric spiralling motions of an incompressible fluid at large Reynolds numbers. By making approximations of the boundary-layer type the Navier-Stokes equations are reduced essentially to a pair of non-linear parabolic equations. Initial conditions are specified on some upstream cross-section, and boundary conditions on the axis of symmetry and on some bounding surface of revolution. The method involves replacing the differential equations by sets of finite-difference equations, using first-order central differences in an implicit scheme. The calculation is by a marching technique, which proceeds step-by-step in the axial direction. For each step an iterative plan is followed. The finite-difference equations themselves are solved by straightforward matrix methods. A programme is developed for a digital computer of moderate size and examples of the application of the method are given. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title A numerical method for solving the equations for a vortex core en_US


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