The steady laminar incompressible boundary-layer problem as an integral equation in crocco variables the calculation of non-similar flows

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dc.contributor.author R. D. Mills en_US
dc.date.accessioned 2014-10-21T15:50:53Z
dc.date.available 2014-10-21T15:50:53Z
dc.date.issued 1973 en_US
dc.identifier.other ARC/R&M-3742 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3020
dc.description.abstract The steady laminar incompressible boundary-layer problem in two dimensions has been posed as an integral equation in Crocco variables in the most general case and an algorithm developed for computing the similarity flows (Mills 1966). The present report extends the algorithm to compute non-similar flows. Essentially it consists of replacing the x-derivative terms in the integral equation by finite differences so that the problem reduces to solving a non-linear integral equation across the boundary layer at successive x-stations starting from an initial solution at x = 0. To obtain convergence a double-field type of iteration with two relaxation factors has to be used. An analysis of the convergence of the process is given in the Appendix. The algorithm was found experimentally to be stable for every combination of step-sizes tried. A local matrix stability analysis of the algorithm is given in the Appendix. A large number of examples have been computed, particularly flows with discontinuous suction distributions, periodic flows and separating flows. For the standard problems the results are in agreement with the known accurate computations. Some new problems are computed. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title The steady laminar incompressible boundary-layer problem as an integral equation in crocco variables the calculation of non-similar flows en_US


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