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Studies of vortex flow aerodynamics using CFD flow visualizationsNavier-Stokes computations of three-dimensional vortical flows over a round-edged double-delta wing and a tangent-ogive forebody are performed using an implicit upwind finite-difference scheme. Computed particle traces are compared with experimental oil-flow streaks.
Document ID
19890057889
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hsu, C.-H. (Vigyan Research Associates, Inc. Hampton, VA, United States)
Hartwich, P.-M. (Vigyan Research Associates, Inc. Hampton, VA, United States)
Liu, C. H. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
August 1, 1989
Subject Category
Aerodynamics
Accession Number
89A45260
Distribution Limits
Public
Copyright
Other

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