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Streamline-curvature effect in three-dimensional boundary layersThe 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.
Document ID
19940035348
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reed, Helen L.
(NASA Langley Research Center Hampton, VA, United States)
Lin, Ray-Sing
(NASA Langley Research Center Hampton, VA, United States)
Petraglia, Media M.
(Arizona State Univ. Tempe, United States)
Date Acquired
August 16, 2013
Publication Date
October 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
SAE PAPER 921987
Meeting Information
Meeting: SAE, Aerotech ''92 Conference
Location: Anaheim, CA
Country: United States
Start Date: October 5, 1992
End Date: October 8, 1992
Sponsors: SAE
Accession Number
94A12003
Distribution Limits
Public
Copyright
Other

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