Laminar boundary layer at a discontinuity in wall curvature

Open Access

1 January 1975

journal article
Published by American Mathematical Society (AMS) in Quarterly of Applied Mathematics

Vol. 33 (2) , 175-181
https://doi.org/10.1090/qam/446071

Abstract

The discontinuity in pressure gradient predicted for two-dimensional inviscid subsonic or supersonic flow at a jump discontinuity in wall curvature is smoothed by means of local solutions which take into account the interaction of a laminar boundary layer with the external flow.

Keywords

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