Streamline - Curvature Effect in Three - Dimensional Boundary Layers
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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. 1992 Society of Automotive Engineers, Inc.
name of conference
Aerospace Technology Conference and Exposition
SAE Technical Paper Series
author list (cited authors)
Reed, H. L., Lin, R., & Petraglia, M. M.