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https://doi.org/10.1017/s0001924000011805
Copy DOIJournal: The Aeronautical Journal | Publication Date: Jan 1, 2003 |
AbstractThe method of matched asymptotic expansions has been applied to analyse the asymptotic structure of the incompressible turbulent attachment-line boundary layer at large Reynolds numbers. Inner and outer solutions were obtained that give the ‘wall-unit’ and ‘velocity-defect’ represention of both the spanwise and chordwise velocity profiles. The predictions from the theory agree with experimental and DNS data in the range of fully developed turbulence.
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