A solution of the laminar boundary-layer equation for retarded flow

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dc.contributor.author D. R. Hartree en_US
dc.date.accessioned 2014-10-21T15:54:14Z
dc.date.available 2014-10-21T15:54:14Z
dc.date.issued 1939 en_US
dc.identifier.other ARC/R&M-2426 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3588
dc.description.abstract The laminar boundary-layer equation, for a linearly retarded velocity in the main stream, U = 1 - 1/8x in reduced variables, has been solved numerically by working in finite intervals in x, with a correction for the finite length of x-interval. The method was first tried out on the region near the forward stagnation point, where the results could be checked from tables given by Howarth, and proved very satisfactory. The separation point has been determined by two independent methods to be close to x = 0.959, in excellent agreement with Howarth's value. The nature of the singularity at the separation point is discussed. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title A solution of the laminar boundary-layer equation for retarded flow en_US


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