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Streamline - Curvature Effect in Three - Dimensional Boundary Layers Arizona State University

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Reed, Helen L., author.
Conference Name:
Aerospace Technology Conference & Exposition (1992-09-23 : Long Beach, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1992
Summary:
AbstractThe 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
Notes:
Vendor supplied data
Publisher Number:
921987
Access Restriction:
Restricted for use by site license

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