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NASA NTRS · 19940035348

Streamline-curvature effect in three-dimensional boundary layers

Abstract

The effect of including wall and streamline curvature terms in swept-wing boundary-layer stability calculations is studied. The linear disturbance equations are cast on a fixed, body-intrinsic, curvilinear coordinate system. Those nonparallel terms which contribute mainly to the streamline-curvature effect are retained in this formulation and approximated by their local finite-difference values. Convex-wall curvature has a stabilizing effect, while streamline curvature is destabilizing if the curvature exceeds a critical value.

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BibTeXRIS

Reed, Helen L., Lin, Ray-Sing, Petraglia, Media M.. 1992-10-01. Streamline-curvature effect in three-dimensional boundary layers. https://ntrs.nasa.gov/citations/19940035348

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