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Careful numerical study of flowfields about asymmetric external conical cornersA numerical study of the flowfield about asymmetrical external axial corners formed by the juncture of swept compressive wedges is presented. The geometrical configuration allows a unified treatment of external corners typical of delta wings and rectangular inlets. The study investigates how the flow transitions from a symmetrical flowfield with a cross-flow stagnation point at the corner to an asymmetrical flowfield for which the flow spills over the corner. The effects of leading-edge sweep, wedge compression, and corner radius are investigated.
Document ID
19800057392
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Salas, M. D. (NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 10, 2013
Publication Date
July 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 80-1329
Meeting Information
Meeting: Fluid and Plasma Dynamics Conference
Location: Snowmass, CO
Start Date: July 14, 1980
End Date: July 16, 1980
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
80A41562
Distribution Limits
Public
Copyright
Other

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