| 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 |